gas turbine engines outlook/ specifications turbine engines general data arrangement performance...

Gas Turbine Engines GENERALDATA ARRANGEMENT PERFORMANCE DIMENSIONS&WTS.

MODEL TYPE APPLICATIONS/ DESIGNATION REMARKS

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*Note: First or first two letters designate compressor type: A=axial, C=centrifugal. Final letter or letters define output: F=fan, J=jet, LJ=lift-jet, P=propeller, PF=propfan, S=shaft.**Combustor type: An=annular, Cn=can-annular, Ca=can.

accurate automation corp., Chattanooga, TN, USAAT-1500 C-J 1 1 An 150 lb. t. 1.35 3.8 8.8 14.5 18 Decoys, targets, UAVs.AT-1700 C-J 1 1 An 210 lb. t. 1.1 4.5 8.8 14.5 19 Decoys, targets, UAVs and USVs.AT-1700-F C-J 1 1, 1 An 320 lb. t. 0.54 6.3 13.5 19 23 Decoys, targets, UAVs and USVs.cfe co. (General electric, Honeywell), Phoenix, AZ, USACFE 738-1-1B AC-F 1, 5, 1 2, 3 An 5,918 lb. t. 0.369 23 48 99 1,325 Falcon 2000, GE/Honeywell joint program.

cfm international (General electric, Snecma), Cincinnati, OH, USACFM56-2A2 A-F 1, 3, 9 1, 4 An 24,000 lb. t. 0.376 25.4 72 95.7 4,820 E-3, E-6, KE-3.CFM56-2B1 (F108) A-F 1, 3, 9 1, 4 An 22,000 lb. t. 0.366 23.7 72 95.7 4,617 C-135FR, KC-135R.CFM56-2C1/C3 A-F 1, 3, 9 1, 4 An 22,000 lb. t. 0.366 24.7 72 95.7 4,635 DC-8 Super 71/72/73.CFM56-2C5/C6 A-F 1, 3, 9 1, 4 An 22,000 lb. t. 0.366 24.7/30.1 72 95.7 4,635 DC-8 Super 71/72/73.CFM56-3B1 A-F 1, 3, 9 1, 4 An 20,000 lb. t. 0.386 22.6 63 93.1 4,290 737-300/500.CFM56-3B2 A-F 1, 3, 9 1, 4 An 22,000 lb. t. 0.396 24.3 63 93.1 4,301 737-300/400.CFM56-3C1 A-F 1, 3, 9 1, 4 An 23,500 lb. t. 0.396 25.2 63 93.1 4,301 737-400.CFM56-5A1 A-F 1, 3, 9 1, 4 An 25,000 lb. t. 0.3316 26.5 72 98.9 4,995 A320.CFM56-5A3 A-F 1, 3, 9 1, 4 An 26,500 lb. t. 0.3316 27.8 72 98.9 4,995 A320.CFM56-5A4 A-F 1, 3, 9 1, 4 An 22,000 lb. t. 0.3316 24.1 72 98.9 4,995 A319.CFM56-5A5 A-F 1, 3, 9 1, 4 An 23,500 lb. t. 0.3316 25.4 72 98.9 4,995 A319.CFM56-5B1/3 A-F 1, 4, 9 1, 4 An 30,000 lb. t. 0.3496 31 72 102.4 5,250 A321.CFM56-5B1/P A-F 1, 4, 9 1, 4 An 30,000 lb. t. 0.3496 31 72 102.4 5,250 A321.CFM56-5B2/3 A-F 1, 4, 9 1, 4 An 31,000 lb. t. 0.3516 31.9 72 102.4 5,250 A321.CFM56-5B2/P A-F 1, 4, 9 1, 4 An 31,000 lb. t. 0.3516 31.9 72 102.4 5,250 A321.CFM56-5B3/3 A-F 1, 4, 9 1, 4 An 32,000 lb. t. 0.3536 33.7 72 102.4 5,250 A320 or A321.CFM56-5B3/P A-F 1, 4, 9 1, 4 An 32,000 lb. t. 0.3536 33.7 72 102.4 5,250 A320 or A321.CFM56-5B4/3 A-F 1, 4, 9 1, 4 An 27,000 lb. t. 0.3356 28.1 72 102.4 5,250 A320.CFM56-5B4/P A-F 1, 4, 9 1, 4 An 27,000 lb. t. 0.3356 28.1 72 102.4 5,250 A320.CFM56-5B5/3 A-F 1, 4, 9 1, 4 An 22,000 lb. t. 0.3266 24.5 72 102.4 5,250 A319 or A320.CFM56-5B5/P A-F 1, 4, 9 1, 4 An 22,000 lb. t. 0.3266 24.5 72 102.4 5,250 A319 or A320.CFM56-5B6/3 A-F 1, 4, 9 1, 4 An 23,500 lb. t. 0.3276 25.9 72 102.4 5,250 A319 or A320.CFM56-5B6/P A-F 1, 4, 9 1, 4 An 23,500 lb. t. 0.3276 25.9 72 102.4 5,250 A319 or A320.CFM56-5B7/3 A-F 1, 4, 9 1, 4 An 27,000 lb. t. 0.3356 28.1 72 102.4 5,250 A319.CFM56-5B7/P A-F 1, 4, 9 1, 4 An 27,000 lb. t. 0.3356 28.1 72 102.4 5,250 A319.CFM56-5B8/3 A-F 1, 4, 9 1, 4 An 21,600 lb. t. 0.3266 24.1 72 102.4 5,250 A318.CFM56-5B8/P A-F 1, 4, 9 1, 4 An 21,600 lb. t. 0.3266 24.1 72 102.4 5,250 A318.CFM56-5B9/3 A-F 1, 4, 9 1, 4 An 23,300 lb. t. 0.3276 25.7 72 102.4 5,250 A318.CFM56-5B9/P A-F 1, 4, 9 1, 4 An 23,300 lb. t. 0.3276 25.7 72 102.4 5,250 A318.CFM56-5C2 A-F 1, 4, 9 1, 5 An 31,200 lb. t. 0.326 28.4 76.6 103 5,670 A340-200/300.CFM56-5C3/P A-F 1, 4, 9 1, 5 An 32,500 lb. t. 0.326 29.5 76.6 103 5,670 A340-200/300.CFM56-5C4/P A-F 1, 4, 9 1, 5 An 34,000 lb. t. 0.336 31 76.6 103 5,670 A340-200/300.CFM56-7B18 A-F 1, 3, 9 1, 4 An 19,500 lb. t. 0.356 21.7 65 98 5,234 737-600.CFM56-7B18/3 A-F 1, 3, 9 1, 4 An 19,500 lb. t. 0.356 21.7 65 98 5,234 737-600.CFM56-7B20 A-F 1, 3, 9 1, 4 An 20,600 lb. t. 0.366 22.7 65 98 5,234 737-600/700.CFM56-7B20/3 A-F 1, 3, 9 1, 4 An 20,600 lb. t. 0.366 22.7 65 98 5,234 737-600/700.CFM56-7B22 A-F 1, 3, 9 1, 4 An 22,700 lb. t. 0.366 24.6 65 98 5,234 737-600/700.CFM56-7B22/3 A-F 1, 3, 9 1, 4 An 22,700 lb. t. 0.366 24.6 65 98 5,234 737-600/700.CFM56-7B24 A-F 1, 3, 9 1, 4 An 24,200 lb. t. 0.376 26 65 98 5,234 737-700/800.CFM56-7B24/3 A-F 1, 3, 9 1, 4 An 24,200 lb. t. 0.376 26 65 98 5,234 737-700/800.CFM56-7B26 A-F 1, 3, 9 1, 4 An 26,300 lb. t. 0.386 27.9 65 98 5,234 737-700/800/900.CFM56-7B26/3 A-F 1, 3, 9 1, 4 An 26,300 lb. t. 0.386 27.9 65 98 5,234 737-700/800/900.CFM56-7B27 A-F 1, 3, 9 1, 4 An 27,300 lb. t. 0.386 28.9 65 98 5,234 737-700/800/900.CFM56-7B27/3 A-F 1, 3, 9 1, 4 An 27,300 lb. t. 0.386 28.9 65 98 5,234 737-700/800/900.enGine alliance (General electric, pratt & Whitney), USA

GP7270 A-F 1, 5, 9 2, 6 An 70,000 lb. t. — 36.1 124 186 13,416 A380-800. MTU 22.5%, Snecma 10%, Tech Space Aero 5%. GP7277 A-F 1, 5, 9 2, 6 An 76,500 lb. t. — 38.6 124 186 13,416 A380-800F. MTU 22.5%, Snecma 10%, Tech Space Aero 5%.

GENERALDATA ARRANGEMENT PERFORMANCE DIMENSIONS&WTS.


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128 aviation week & space technology/January 28, 2008 www.aviationweek.com/awst

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Gas Turbine Engines




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epi europrop international GmBH. (itp, mtu aero engines, rolls-royce, Snecma), Munich, GermanyTP400-D6 A-P 1, 5, 6 1, 1, 3 An 11,000 shp. — 25 — 138 3,970 A400M.eurojet (avio, itp, mtu aero engines, rolls-royce), Hallbergmoos, Germany

EJ200 A-F 3, 5 1, 1 An 20,000 lb. t. A/B 1.69 26 29 157 2,180 Typhoon.General electric co., Ge transportation - aircraft engines, Cincinnati, OH, USA

CF6-6D1A A-F 1, 1, 16 2, 5 An 41,500 lb. t. 0.35 25.2 105 188 8,966 DC-10-10.CF6-6K/K2 A-F 1, 1, 16 2, 5 An 41,500 lb. t. 0.346 25 105 188 8,176 DC-10-10.CF6-50C1 A-F 1, 3, 14 2, 4 An 51,000 lb. t. 0.39 29.3 105 183 8,966 A300B, DC-10-30, KC-10. Snecma has 10% share.CF6-50C2 A-F 1, 3, 14 2, 4 An 52,500 lb. t. 0.371 30.4 105 183 8,966 KC-10.CF6-50C2B A-F 1, 3, 14 2, 4 An 54,000 lb. t. 0.385 31.1 105 183 8,966 DC-10-30. Snecma has 10% share.CF6-50C2R A-F 1, 3, 14 2, 4 An 51,000 lb. t. 0.368 29.2 105 183 8,966 A300B, DC-10-30. Snecma has 10% share.CF6-50E/E1 A-F 1, 3, 14 2, 4 An 52,500 lb. t. 0.376 30.1 105 183 9,047 747-200. Snecma has 10% share.CF6-50E2 A-F 1, 3, 14 2, 4 An 52,500 lb. t. 0.371 30.4 105 183 9,047 747-200, E-4. Snecma has 10% share.CF6-50E2B A-F 1, 3, 14 2, 4 An 54,000 lb. t. 0.375 30.9 105 183 9,047 747-200. Snecma has 10% share.CF6-80A A-F 1, 3, 14 2, 4 An 48,000 lb. t. 0.344 27.3 98 167 8,776 767-200. Snecma has 10% share.CF6-80A2 A-F 1, 3, 14 2, 4 An 50,000 lb. t. 0.352 28.4 98 167 8,776 767-200. Snecma has 10% share.CF6-80A3 A-F 1, 3, 14 2, 4 An 50,000 lb. t. 0.352 28.4 106 167 8,760 A310-200. Snecma has 10% share.CF6-80C2A1 A-F 1, 4, 14 2, 5 An 59,000 lb. t. 0.334 30.4 106 168 9,480 A300-600. MTU has 9.1% share, Snecma 10%.CF6-80C2A2 A-F 1, 4, 14 2, 5 An 53,500 lb. t. 0.324 27.8 106 168 9,480 A310-200 Adv., A310-300. Snecma has 10% share.CF6-80C2A3 A-F 1, 4, 14 2, 5 An 60,200 lb. t. 0.337 31.1 106 168 9,480 A300-600, MD-11. Snecma has 10% share.CF6-80C2A5 A-F 1, 4, 14 2, 5 An 61,300 lb. t. 0.34 31.5 106 168 9,480 A300-600R. Snecma has 10% share.CF6-80C2A5F A-F 1, 4, 14 2, 5 An 61,300 lb. t. 0.34 31.5 106 168 9,860 A300-600F. Snecma has 10% share.CF6-80C2A8 A-F 1, 4, 14 2, 5 An 59,000 lb. t. 0.344 30.4 106 168 9,480 A310-200 Adv., A310-300. Snecma has 10% share.CF6-80C2B1 A-F 1, 4, 14 2, 5 An 56,700 lb. t. 0.339 29.3 106 168 9,670 747-300. Snecma has 10% share.CF6-80C2B1F A-F 1, 4, 14 2, 5 An 58,090 lb. t. 0.337 29.9 106 168 9,790 747-400. Snecma has 10% share.CF6-80C2B2 A-F 1, 4, 14 2, 5 An 52,500 lb. t. 0.33 27.4 106 168 9,670 767-200. Snecma has 10% share.CF6-80C2B2F A-F 1, 4, 14 2, 5 An 52,700 lb. t. 0.329 27.4 106 168 9,790 767-300ER. Snecma has 10% share.CF6-80C2B4 A-F 1, 4, 14 2, 5 An 57,900 lb. t. 0.341 29.9 106 168 9,670 767-200ER/300/300ER. Snecma has 10% share.CF6-80C2B4F A-F 1, 4, 14 2, 5 An 58,100 lb. t. 0.337 29.9 106 168 9,790 767-300ER. Snecma has 10% share.CF6-80C2B5F A-F 1, 4, 14 2, 5 An 60,800 lb. t. 0.342 31.4 111 168 9,790 747-400ER.CF6-80C2B6 A-F 1, 4, 14 2, 5 An 60,800 lb. t. 0.348 31.1 106 168 9,670 767-300ER. Snecma has 10% share.CF6-80C2B6F A-F 1, 4, 14 2, 5 An 60,800 lb. t. 0.342 31.4 111 168 9,790 767 Global Tanker/Transport.CF6-80C2B6FA A-F 1, 4, 14 2, 5 An 60,800 lb. t. 0.343 31.4 106 168 9,847 767 AWACS. Snecma has 10% share.CF6-80C2B7F A-F 1, 4, 14 2, 5 An 60,800 lb. t. 0.342 31.4 111 168 9,790 767-200ER/300ER/400ER. Snecma has 10% share.CF6-80C2B8F A-F 1, 4, 14 2, 5 An 60,800 lb. t. 0.35 31.4 106 168 9,970 767-400ER. Snecma has 10% share.CF6-80C2D1F A-F 1, 4, 14 2, 5 An 61,960 lb. t. 0.339 32.2 106 168 9,850 MD-11. Snecma has 10% share.CF6-80C2K1F A-F 1, 4, 14 2, 5 An 59,740 lb. t. 0.343 31.4 111 168 9,790 Japan C-X TransportCF6-80C2L1F A-F 1, 4, 14 2, 5 An 51,250 lb. t. 0.337 27.1 111 168 9,790 Lockheed Martin C-5M.CF6-80E1A2 A-F 1, 4, 14 2, 5 An 67,500 lb. t. 0.34 32.4 114 168 11,225 A330. MTU has 9.1% share, Snecma 20%.CF6-80E1A3 A-F 1, 4, 14 2, 5 An 72,000 lb. t. 0.345 34.8 114 168 11,225 A330-200/300. Snecma has 20% share.CF6-80E1A4 A-F 1, 4, 14 2, 5 An 70,000 lb. t. 0.345 33.7 114 168 11,225 A330-200/300. Snecma has 20% share.CF6-80E1A4/B A-F 1, 4, 14 2, 5 An 72,000 lb.t. 0.345 34.8 114 168 11,225 A330-200/300. Snecma has 20% share.CF34-1A/3A/3A2 A-F 1, 14 2, 4 An 9,220 lb. t. 0.357 21 49 103 1,625 Bombardier CL601, CL601-3A.CF34-3A1 A-F 1, 14 2, 4 An 9,220 lb. t. 0.357 21 49 103 1,655 Bombardier CRJ100, CL601-3R.CF34-3B/3B1 A-F 1, 14 2, 4 An 9,220 lb. t. 0.346 21 49 103 1,670 Bombardier CL604, CRJ200.CF34-8C1 A-F 1, 10 2, 4 An 13,790 lb. t. 0.37 28 52 128 2,350 Bombardier CRJ700.CF34-8C5 A-F 1, 10 2, 4 An 14,510 lb. t. 0.39 28.5 52 128 2,450 Bombardier CRJ900/1000.CF34-8C5B1 A-F 1, 10 2, 4 An 13,790 lb. t. 0.37 28 52 128 2,410 Bombardier CRJ700.CF34-8E A-F 1, 10 2, 4 An 14,510 lb. t. 0.39 28.5 52 128 2,450 Embraer 170/175.CF34-10A A-F 1, 3, 9 1, 4 An 20,360 lb. t. 0.37 29 57 90 3,700 ACAC ARJ21-700/900CF34-10E A-F 1, 3, 9 1, 4 An 20,360 lb. t. 0.37 29 57 90 3,700 Embraer 190/195.CT7-2A AC-S 5, 1 2, 2 An 1,725 shp. 0.481 17 25 47 429 Bell 214ST.CT7-2D AC-S 5, 1 2, 2 An 1,725 shp. 0.481 17 25 47 442 Sikorsky S-70C.CT7-2D1 AC-S 5, 1 2, 2 An 1,725 shp. 0.481 17 25 47 466 Sikorsky S-70C.CT7-5A2 AC-P 5, 1 2, 2 An 1,735 shp. 0.476 17 29 96 783 Saab 340A.CT7-6/6A AC-S 5, 1 2, 2 An 2,000 shp. 0.457 18 25 48.2 493 EH Industries EH101.CT7-7A AC-P 5, 1 2, 2 An 1,700 shp. 0.474 17 29 96 783 CASA-IPTN CN-235.CT7-8 AC-S 5, 1 2, 2 An 2,520 shp. 0.45 21 26 48.2 537 Sikorsky S-92.CT7-8A AC-S 5, 1 2, 2 An 2,520 shp. 0.45 21 26 48.2 542 Sikorsky S-92, H-92.



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Gas Turbine Engines


CT7-8E AC-S 5, 1 2, 2 An 2,527 shp 0.45 21 26 48.2 542 VH-71A.CT7-9B/9C AC-P 5, 1 2, 2 An 1,870 shp. 0.471 18 29 96 805 CASA-IPTN CN-235-100/200, Saab 340B, Sukhoi Su-80.CT7-9C3 AC-P 5, 1 2, 2 An 1,870 shp. 0.471 18 29 96 807 CASA-IPTN CN-235-300/330.CT7-9D AC-P 5, 1 2, 2 An 1,940 shp. 0.455 18 29 96 805 Let L610G.CT58-140 A-S 10 2, 1 An 1,500 shp. 0.61 8.4 20.7 55 340 Boeing Vertol 107-2, Sikorsky S-6.CT64-820-4 A-P 14 2, 2 An 3,133 shp. 0.49 12.5 20.1 110 1,145 De Havilland DHC-5D.F101-GE-102 A-F 1, 1, 9 1, 2 An 30,780 lb. t. 2.46 26.8 55 181 4,400 US Air Force B-1B.F103-GE-100 (CF6-50E2) A-F 1, 3, 14 2, 4 An 51,800 lb. t. 0.371 30.5 105 183 9,047 E-4B airborne command post.F103-GE-101 (CF6-50C2) A-F 1, 3, 14 2, 4 An 51,800 lb. t. 0.371 30.5 105 183 8,966 KC-10A.F103-GE-102 (CF6-80C2B1) A-F 1, 4, 14 2, 5 An 55,980 lb. t. 0.323 29.3 106 168 9,670 Boeing VC-25A (Air Force One).F110-GE-100 A-F 1, 2, 9 1, 2 An 28,000 lb. t. 2.06 30.4 46.5 182.3 3,920 Lockheed Martin F-16C/D.F110-GE-129 A-F 1, 2, 9 1, 2 An 29,000 lb. t. 1.9 30.7 46.5 182.3 3,950 Boeing F-15E/K, Lockheed Martin F-16C/D, Mitsubishi F-2.F110-GE-132 A-F 1, 2, 9 1, 2 An 32,130 lb. t. 2.09 33.3 46.5 185.3 4,150 Lockheed Martin F-16 Block 60.F110-GE-400 A-F 1, 2, 9 1, 2 An 27,000 lb. t. 2 29.9 46.5 232.3 4,400 Northrop Grumman F-14B/D.F118-GE-100 A-F 1, 2, 9 1, 2 An 19,000 lb. t. — 35.1 46.5 100.5 3,200 Non-AB F110 derivative for Northrop Grumman B-2.F118-GE-101 A-F 1, 2, 9 1, 2 An 17,000 lb. t. — 27 47 110 3,150 Lockheed U-2.F404/F1D2 A-F 3, 7 1, 1 An 10,540 lb. t. 0.8 24 35 83 1,730 Lockheed Martin F-117A.F404/RM12 A-F 3, 7 1, 1 An 18,100 lb. t. 1.78 27 35 154 2,325 Saab JAS 39.F404-GE-100D A-F 3, 7 1, 1 An 11,000 lb. t. 0.81 24 35 89 1,820 Singapore A-4SU.F404-GE-102 A-F 3, 7 1, 1 An 17,700 lb. t. 1.72 26 35 154 2,288 KAI/Lockheed Martin T-50.F404-GE-400 A-F 3, 7 1, 1 An 16,000 lb. t. 1.85 26 35 154 2,225 Boeing F/A-18A/B/C/D.F404-GE-402 A-F 3, 7 1, 1 An 17,700 lb. t. 1.74 26 35 154 2,282 Boeing F/A-18C/D.F404-GE-F2J3 A-F 3, 7 1, 1 An 18,300 lb. t. 1.81 27 35 154 2,335 Indian Light Combat Aircraft fighter.F404-GE-IN20 A-F 3, 7 1, 1 An 18,800 lb. t. 1.78 28 35 154 2,365 Indian Light Combat Aircraft fighter.F414-GE-400 A-F 3, 7 1, 1 An 22,000 lb. t. — 30 35 154 — Boeing F/A-18E/F, EA-18G.GE90-76B A-F 1, 3, 10 2, 6 An 76,000 lb. t. — 40 134 287 17,250 777-200. Snecma, Avio and IHI are

revenue-sharing participants.GE90-85B A-F 1, 3, 10 2, 6 An 84,700 lb. t. — 40 134 287 17,250 777-200/200ER. Snecma, Avio and IHI are

revenue-sharing participants.GE90-90B A-F 1, 3, 10 2, 6 An 90,000 lb. t. — 40 134 287 17,250 777-200/200ER. Snecma, Avio and IHI are

revenue-sharing participants.GE90-94B A-F 1, 3, 10 2, 6 An 93,700 lb. t. — 40 134 287 17,250 777-200ER. Snecma, Avio and IHI are

revenue-sharing participants.GE90-110B A-F 1, 4, 9 2, 6 An 110,000 lb. t. — 42 135 287 19,315 777-200LR. Snecma, Avio and IHI are

revenue-sharing participants.GE90-115B A-F 1, 4, 9 2, 6 An 115,540 lb. t. — 42 135 287 19,315 777-300ER. Snecma, Avio and IHI are

revenue-sharing participants.GEnx-1B75 A-F 1, 4, 10 2, 7 An 53,200 lb. t. — 36 140 195 — Boeing 787-3.GEnx-1B75 A-F 1, 4, 10 2, 7 An 63,800 lb. t. — 41 140 195 — Boeing 787-8.GEnx-1B75 A-F 1, 4, 10 2, 7 An 69,800 lb. t. — 43 140 195 — Boeing 787-9.GEnx-2B67 A-F 1, 3, 10 2, 6 An 66,500 lb. t. — 43 127 185 — Boeing 747-8.J79-GE-8 A-J 17 3 Cn 17,000 lb. t. 1.93 12.9 38.3 208.5 3,695 F-4B/N, RF-4B.J79-GE-10/17 A-J 17 3 Cn 17,820 lb. t. 1.93 13.4 39.1 208.7 3,855 F-4J/G/S/E.J79-GE-15 A-J 17 3 Cn 17,000 lb. t. 1.94 12.9 38.3 208.4 3,699 F-4C/D, RF-4C.J85-GE-4 A-J 8 2 An 2,950 lb. t. 1.01 6.9 17.7 40.5 404 Rockwell T-2C.J85-GE-5J A-J 8 2 An 3,850 lb. t. 2.2 6.7 21 104.6 584 Afterburner. Northrop Grumman T-38A.J85-GE-13 A-J 8 2 An 4,087 lb. t. 2.2 6.8 21 104.6 597 Afterburner. Northrop Grumman F-5A/B.J85-GE-17A/B A-J 8 2 An 2,850 lb. t. 0.99 6.9 17.7 40.5 400 Cessna A-37A/B, CL41G, Saab 105XT.J85-GE-21 A-J 8 2 An 5,000 lb. t. 2.13 8.3 26.1 117 684 Afterburner. Northrop Grumman F-5E.T58-GE-8F A-S 10 2, 1 An 1,350 shp. 0.6 8.2 20.2 55 305 Sikorsky S-61A-1.T58-GE-16 A-S 10 2, 2 An 1,870 shp. 0.53 8.4 24.2 64 443 Boeing CH-46E.T58-GE-100 A-S 10 2, 1 An 1,500 shp. 0.61 8.4 20.9 55 335 Sikorsky CH-124 Sea King, S-61A-4, HH-3E, SH-3D.T58-GE-400B A-S 10 2, 1 An 1,500 shp. 0.61 8.4 20.9 55 345 Sikorsky VH-3D.T58-GE-402 A-S 10 2, 1 An 1,500 shp. 0.61 8.4 20.2 55 345 Boeing CH-46D, HH-46D, Sikorsky SH-3H, UH-3H, UH-46D.T64/P4D A-P 14 2, 2 An 3,400 shp. 0.49 13.2 20.1 110 1,188 Alenia G.222, C-27A.T64-GE-7A A-S 14 2, 2 An 3,936 shp. 0.47 14.1 20.1 79 720 Sikorsky CH/HH-53C.T64-GE-100 A-S 14 2, 2 An 4,330 shp. 0.48 14.9 20.1 79 720 Sikorsky MH-53J/M/TH-53A, S-65A/H-53.T64-GE-413A A-S 14 2, 2 An 3,925 shp. 0.47 14.1 20.1 79 710 Sikorsky CH-53D.



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Gas Turbine Engines


T64-GE-415/416/416A A-S 14 2, 2 An 4,380 shp. 0.48 14.8 20.1 79 720 Sikorsky CH-53E, RH-53D/E.T64-GE-419 A-S 14 2, 2 An 4,750 shp. 0.47 14.9 20.1 79 755 Sikorsky MH-53E.T700-GE-401 AC-S 5, 1 2, 2 An 1,690 shp. 0.464 17 25 47 443 Bell AH-1W, Sikorsky HH-60D, SH-2G, SH-60B.T700-GE-401C AC-S 5, 1 2, 2 An 1,800 shp. 0.46 18 25 47 458 Sikorsky HH-60H/J, MH-60R, SH-60B/F.T700-GE-700 AC-S 5, 1 2, 2 An 1,622 shp. 0.465 17 25 47 437 Sikorsky EH-60A, MH-60G, UH-60A.T700-GE-701 AC-S 5, 1 2, 2 An 1,698 shp. 0.464 17 25 47 438 Boeing AH-64.T700-GE-701A AC-S 5, 1 2, 2 An 1,723 shp. 0.465 17 25 47 438 Sikorsky S-70C.T700-GE-701C AC-S 5, 1 2, 2 An 1,890 shp. 0.462 18 25 47 456 AH-64, MH-60G, MH-60K, UH-1Y, UH-60L.T700-GE-701D AC-S 5, 1 2, 2 An 2,000 shp. 0.462 18 25 47 456 Boeing AH-64, Sikorsky UH-60M.T700/T6A AC-S 5, 1 2, 2 An 2,000 shp. 0.45 18 25 48.2 485 Italian navy EH101.T700/T6A1 AC-S 5, 1 2, 2 An 2,145 shp. 0.445 19 25 48.2 493 Canadian EH101.T700/T6E AC-S 5, 1 2, 2 An 2,380 shp. 0.433 19 26 48 531 NH Industries NH90.T700/T6E1 AC-S 5, 1 2, 2 An 2,269 shp. 0.439 19 25 48 537 NH Industries NH90.TF34-GE-100A A-F 1, 14 2, 4 An 9,065 lb. t. 0.371 21 49 100 1,440 Fairchild Republic A-10.TF34-GE-400B A-F 1, 14 2, 4 An 9,275 lb. t. 0.363 21 52 100 1,478 Lockheed S-3A.TF39-1C A-F 1.5, 16 2, 6 An 43,000 lb. t. 0.313 8 97 312 7,996 Lockheed Martin C-5A, C-5B, C-5C.Ge Honda aero enGineS, Cincinnati, OH, USA

HF120 C-F — — An 2,095 lb. t. — — — — — HondaJet, Spectrum 40.Ge rollS-royce fiGHter enGine team, Cincinnati, OH, USA

F136-GE-100 A-F 3, 5 1, 3 An 40,800 lb. t. — — 48 221 — Lockheed Martin CTOL F-35A.F136-GE-400 A-F 3, 5 1, 3 An 40,800 lb. t. — — 48 221 — Lockheed Martin Naval CV F-35C.F136-GE-600 A-F 3, 5 1, 3 An 39,400 lb. t. — — 48 221 — Lockheed Martin Stovl F-35B.HoneyWell, Phoenix, AZ, USA

AL5512 AC-S 7, 1 2, 2 An 4,075 shp. 0.52 8.2 24 47 770 Civil T55-L-712. Boeing Helo Model 234.ALF502L/L-2 AC-F 3, 7, 1 2, 2 An 7,500 lb. t. 0.428 13.7 50 65.6 1,311 Canadair Challenger 600.ALF502L-2A/2C/3 AC-F 3, 7, 1 2, 2 An 7,500 lb. t. 0.414 13.8 50 65.6 1,311 Canadair Challenger 600.ALF502R-3 AC-F 2, 7, 1 2, 2 An 6,700 lb. t. 0.411 11.6 50 63.8 1,336 BAe 146.ALF502R-5 AC-F 2, 7, 1 2, 2 An 6,970 lb. t. 0.408 12.2 50 63.8 1,336 BAe 146.ALF502R-6 AC-F 3, 7, 1 2, 2 An 7,500 lb. t. 0.415 13.8 50 65.6 1,375 BAe 146.AS907 AC-F 1, 4, 1 2, 3 An 6,500 lb. t. 0.42 21 46.3 92.4 1,364 Bombardier Challenger 300.AS977 AC-F 1, 4, 1 2, 3 An 7,092 lb. t. 0.416 23 49.9 92.4 1,364 —ATF 3-3 AC-F 1, 5, 1 1, 3, 2 An 5,440 lb. t. 0.506 22.8 33.9 103.2 1,118 HU-25A.ATF 3-6A AC-F 1, 5, 1 1, 3, 2 An 5,440 lb. t. 0.503 21.3 33.9 102.3 1,125 Falcon 200, French Guardian.F109-GA-100 AC-F 1, 2 2, 2 An 1,330 lb. t. 0.396 20.7 30.7 44.5 439 Squalus.F124-GA-100 AC-F 3, 5 1, 1 — 6,300 lb. t. 0.81 19.4 36 66.8 1,100 Selected for Aero Vodochody L-159.LF507-1F AC-F 3, 7, 1 2, 2 An 7,000 lb. t. 0.397 13.8 50 65.6 1,385 Fadec-equipped Avro RJ series.LF507-1H AC-F 3, 7, 1 2, 2 An 7,000 lb. t. 0.406 13.8 50 65.6 1,375 Avro RJ transport w/hydromechanical fuel control.LTC4B-8D AC-S 7, 1 1, 2 An 2,250 shp. 0.63 6 24 44 605 Military version of T5508D.LTS101-600A-3/-3A AC-S 1, 1 1, 1 An 615/650 shp. 0.58 8.4 22.4 31 253 Eurocopter AS350D/AS350.LTS101-650B-1 AC-S 1, 1 1, 1 An 650 shp. 0.57 8.4 25.4 31 266 Eurocopter/KHI BK-117A helicopter.LTS101-650C-3/3A AC-S 1, 1 1, 1 An 675 shp. 0.57 8.4 22.6 31 241 Bell 222.LTP101-700A-1A AC-P 1, 1 1, 1 An 700 eshp. 0.55 8.6 21 36 335 Piaggio P-166, Riley/Cessna 421.LTS101-750B-1 AC-S 1, 1 1, 1 An 727 shp. 0.57 8.4 25.4 31 271 Eurocopter/KHI BK-117-B.LTS101-750B-2 AC-S 1, 1 1, 1 An 742 shp. 0.57 8.8 24.7 32.4 268 Eurocopter HH-65A SRR.LTS101-750C-1 AC-S 1, 1 1, 1 An 735 shp. 0.57 8.8 22.6 31 244 Bell 222B.T53-13B AC-S 5, 1 2, 2 An 1,400 shp. 0.58 7 23 47.6 544 Bell 205 series.T53-A-17A AC-S 5, 1 2, 2 An 1,500 shp. 0.59 7 23 47.6 545 Kaman K-Max.T53-L-13B AC-S 5, 1 2, 2 An 1,400 shp. 0.58 7 23 47.6 545 Bell UH-1H.T53-L-701A AC-P 5, 1 2, 2 An 1,400 shp. 0.59 7 23 59.4 693 Northrop Grumman OV-1, TCH-1A.T53-L-703 AC-S 5, 1 2, 2 An 1,800 shp. 0.568 8 23 47.6 545 AH-1S, Bell AH-1Q.T55-GA-714A AC-S 7, 1 2, 2 An 4,777 shp. 0.51 9.3 28.7 48.5 879 CH-47D/F.T55-L-712 AC-S 7, 1 2, 2 An 3,750 shp. 0.52 8.2 28.7 48.5 760 CH-47D.T55-L-714 AC-S 7, 1 2, 2 An 4,867 shp. 0.5 9.3 28.7 48.5 832 MH-47.T55-L-714A AC-S 7, 1 2, 2 An 4,868 shp. 0.5 9.3 28.7 48.5 832 CH-47F.T76-G-10/-12/-400 Series C-P 2 3 An 1,040 shp. 0.6 8.5 26 43 320/360 Northrop Grumman OV-10.TFE731-2 AC-F 1, 4, 1 1, 3 An 3,500 lb. t. 0.504 13 39.4 49.7 734 CASA C-101EB, Falcon 100, Lear 35/36, others.TFE731-3 AC-F 1, 4, 1 1, 3 An 3,700 lb. t. 0.511 14.6 39.4 49.7 742 BAe 125-700, IAI 1124, Jetstar, others.



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www.aviationweek.com/awst aviation week & space technology/January 28, 2008 135

TFE731-3A AC-F 1, 4, 1 1, 3 An 3,700 lb. t. 0.515 14.6 39.4 49.7 766 Astra, Lear 55.TFE731-3B AC-F 1, 4, 1 1, 3 An 3,650 lb. t. 0.507 14.4 39.4 49.7 750 Citation III/VI.TFE731-4 AC-F 1, 4, 1 1, 3 An 4,080 lb. t. 0.517 14.8 39.4 51 822 Citation VII.TFE731-5 AC-F 1, 4, 1 1, 3 An 4,304 lb. t. 0.484 14.6 40.5 54.7 852 BAe 125-800, CASA C-101CC.TFE731-5AR AC-F 1, 4, 1 1, 3 An 4,500 lb. t. 0.469 14.6 40.5 80.8 884 Falcon 20 retrofit, Falcon 900.TFE731-5BR AC-F 1 ,4, 1 1, 3 An 4,750 lb. t. 0.47 15.1 40.5 80.8 899 Falcon 20 retrofit, Falcon 900B, Hawker 800XP.TFE731-20 AC-F 1 ,4, 1 1, 3 An 3,650 lb. t. 0.441 21 39.4 51 885 Learjet 45.TFE731-40 AC-F 1 ,4, 1 1, 3 An 4,250 lb. t. 0.457 22 39.4 51 885 Falcon 50EX, IAI Astra SPX.TFE731-60 AC-F 1 ,4, 1 1, 3 An 5,000 lb. t. 0.405 22 42.4 72 988 Falcon 900EX.TFE1042 (F125-GA-100) AC-F 3, 5 1, 1 An 9,400 lb. t. 1.97 19.7 36 140.2 1,360 Taiwanese Indigenous Defense Fighter.TPE331-1 C-P 2 3 An 665 shp. 0.571 8.3 26 43 335 Comm. 680, Fairchild Porter, Merlin 2B, MU-2.TPE331-2 C-P 2 3 An 715 shp. 0.556 8.3 26 43 335 CASA C-212, Shorts Skyvan.TPE331-3/3U C-P 2 3 An 840 shp. 0.548 10.3 26 43 355 Merlin 3/4, Metro 2.TPE331-5 Series C-P 2 3 An 776 shp. 0.577 10.3 26 43 355 CASA C-212, Com. 690, Do 228, MU-2.TPE331-6 Series C-P 2 3 An 715 shp. 0.577 10.3 26 43 355 Beech B100, Merlin 2B, MU-2, Skyvan.TPE331-8/9 C-P 2 3 An 715/865 shp. 0.568 10.3 26 43 370 Cessna Conquest.TPE331-10 Series C-P 2 3 An 940 shp. 0.55 10.8 26 46 385 CASA C-212, Jetstream 31, Merlin 300, MU-2.TPE331-11 C-P 2 3 An 1,000 shp. 0.53 10.8 26 46 400 FMA Pucara, Merlin 4C, Metro 3.TPE331-12B C-P 2 3 An 1,100 shp. 0.522 10.8 26 46 420 Tucano.TPE331-12JR/12UAR/12UHR C-P 2 3 An 1,100 shp. 0.522 10.8 26 46 390 CASA C-212, Jetstream Super 31, Metro 23.TPE331-14A/B/F/UA/UB C-P 2 3 An 1,645 shp. 0.515 11 32 53 585 Piper Cheyenne 400LS.TPE331-14GR/HR C-P 2 3 An 1,759 shp. 0.51 11.4 36 53 633 Antonov An-38, Jetstream 41.TPE331-15AW C-P 2 3 An 1,645 shp. 0.505 11 32 53 622 Northrop Grumman S-2.TPF331-25/43/47/55/ 61 Series

C-P 2 3 An 575 shp. 0.665 8.2 26 46 335 Mitsubishi MU-2, Rockwell Turbo Commander 68/681, Turbo 18/Turboliner, Volpar.

international aero enGineS aG (japanese aero engine consortium, mtu aero engines, pratt & Whitney, rolls-royce), East Hartford, CT, USAV2500-A1 A-F 1, 3, 10 2, 5 An 25,000 lb. t. 0.35 29.8 63 126 5,210 A320-231. V2522-A5 A-F 1, 4, 10 2, 5 An 23,000 lb. t. 0.34 26.9 63.5 126 5,210 A319-131.V2524-A5 A-F 1, 4, 10 2, 5 An 24,500 lb. t. 0.36 26.9 63.5 126 5,210 A319-132.V2525-D5 A-F 1, 4,1 0 2.5 An 28,600 lb. t. 0.35 30.0 63.5 126 5,610 MD-90-30.V2527-A5 A-F 1, 4, 10 2, 5 An 26,600 lb. t. 0.36 27.2 63.5 126 5,210 A320-232.V2527E-A5 A-F 1, 4, 10 2, 5 An 26,600 lb. t. 0.36 27.2 63.5 126 5,210 A320-233.V2527M-A5 A-F 1, 4, 10 2, 5 An 26,600 lb. t. 0.36 27.2 63.5 126 5,210 A319CJ, A319-133.V2528-D5 A-F 1, 4, 10 2, 5 An 28,600 lb. t. 0.35 30.0 63.5 126 5,610 MD-90-30ER.V2530-A5 A-F 1, 4, 10 2, 5 An 30,400 lb. t. 0.36 32.1 63.5 126 5,210 A321-131.V2533-A5 A-F 1, 4, 10 2, 5 An 32,000 lb. t. 0.36 33.4 63.5 126 5,210 A321-231.iSHikaWajima-Harima Heavy induStrieS, Tokyo, Japan

CT58-IHI-140-1 A-S 10 1, 2 An 1,400 shp. 0.61 8.4 20.9 59 340 Kawasaki KV-107A.F3-IHI-30/-30B A-F 2, 5 1, 2 An 3,682 lb. t. 0.7 11 24.8 79 750 Kawasaki T-4.F100-IHI-100 A-F 3, 10 2, 2 An 23,830 lb. t. 2.21 24.9 46.5 198.3 3,068 Japanese F-15J/DJ.F100-IHI-220E A-F 3, 10 2, 2 An 23,450 lb. t. 2.26 25.3 46.5 208.1 3,179 Japanese F-15J/DJ.F110-IHI-129 A-F 3, 9 1, 2 An 29,000 lb. t. 1.9 30.7 46.5 182.3 3,940 Mitsubishi F-2.J3-IHI-7B A-J 8 1 Cn 3,086 lb. t. 1.06 4.5 24.8 82 838 Fuji T-1BJ79-IHI-17 A-J 17 3 Cn 17,900 lb. t. 1.97 13.4 39 209 3,846 Mitsubishi F-4.T56-IHI-14 A-P 14 4 Cn 4,910 eshp. 0.535 9.5 31.4 146 1,890 Japanese P-3C.T64-IHI-10J A-P 14 2, 2 An 3,493 eshp. 0.489 12.5 21 113 1,240 US-1A, YS-11E.T700-IHI-401C AC-S 5, 1 2, 2 An 1,940 shp. 0.465 18 25 46 458 SH-60J, UH-60J, UH-60JA.TF40-IHI-801A A-F 2, 5 1, 1 An 7,300 lb. t. 0.74 11 30 114 1,685 Mitsubishi F-1, T-2.

ivcHenko-proGreSS deSiGn Bureau, Zaporozhye, UkraineAI-20, Series 5 A-P 10 3 An 5,180 eshp. 0.5 7.7 46.5 121.9 2,293 An-8/10/2/32, Beriev Be-12, Il-18/20/22/38. AI-22 A-F 1, 5, 7 3, 1 An 8,422 lb. t. 0.882 15.6 61 118.5 1,687 Tupolev Tu-324, Yakovlev Yak-48.AI-24 A-P 10 3 An 6,217 eshp. 0.562 6.5 42.3 92.4 1,323 Antonov An-24, An-26, An-30. AI-25 A-F 3, 8 2, 1 An 3,307 lb. t. 1.235 8.1 35.3 78.5 688 Yakovlev Yak-40.AI-25TL A-F 3, 9 2, 1 An 3,792 lb. t. 1.279 9.5 38.8 132.2 772 Aero Vodochody L-39.AI-25TLK A-F 3, 9 2, 1 An 3,792 lb. t. 1.279 9.5 38.8 112.6 772 Avic II JL-8.AI-25TLSh A-F 3, 9 2, 1 An 4,079 lb. t. 1.323 10 38.8 132.2 772 Aero Vodochody L-39U.AI-222-25 A-F 2, 8 1, 1 An 5,512 lb. t. 1.411 15.3 42.7 91.3 970 Yakovlev Yak-130.



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OUTLOOK/SPECIFICATIONS

COMMERCIALSATELLITE OPERATORS

WORLD MILITARY

AIRCRAFT INVENTORYMAJOR AIRLINE PROFILES

PRIME CONTRACTOR AND MAJORMANUFACTURER PROFILES

LEADING ALL-CARGO AIRLINES

Gas Turbine Engines


AI-222-28 A-F 2, 8 1, 1 An 6,173 lb. t 1.493 16.6 42.6 88.1 992 Yakovlev Yak-133.AI-222-40 A-F 2, 8 1, 1 An 9,149 lb. t. 0.84 13.6 61 118.5 1,598 UAV.AI-222K-25F A-F 2, 8 1, 1 An 9,259 lb. t. A/B 4.188 15.4 43.9 147.6 1,235 AVIC II L-15.AI-450 C-S 1 1, 1 An 465 shp. 0.573 7.3 21.1 42.7 227 Mil Mi-2A, Kamov Ka-226.AI-450-2 C-S 1 1, 1 An 630 shp. 0.551 7.5 26.8 43.9 309 Ansat. Kazan Helicopter Plant.AI-450M C-S 1 1, 1 An 465 shp. 0.573 7.6 26.9 49.4 265 Mil Mi-2AM.AI-450TP C-P 1 1, 1 An 500 shp. 0.551 7.5 27.6 40.9 271 Yakovlev Yak-152, Sukhoi K-2 UAV, Beriev Be-103.AI-727M AC-F 1, 5, 3 3, 1, 1 An 22,046 lb. t. 0.584 24.7 88.6 126 4,960 Airliner, transport airplane.D-18T A-F 1, 7, 7 4, 1, 1 An 51,655 lb. t. 0.761 23 115.6 212.6 9,039 Antonov An-124, An-124-100, An-225. D-18T, Series 4 A-F 1, 7, 7 4, 1, 1 An 56,946 lb. t. 0.798 24.8 115.6 212.6 9,149 Antonov An-124-100M-150.D-27 AC-PF 5, 3 4, 1, 1 An 14,000 eshp. 0.375 22.9 53.9 165.3 3,638 Antonov An-70.D-36, Series 1 A-F 1, 6, 7 3, 1, 1 An 14,330 lb. t. 0.805 18.9 67.4 136.6 2,478 Yakovlev Yak-42.D-36, Series 1A A-F 1, 6, 7 3, 1, 1 An 14,330 lb. t. 0.805 18.9 67.4 125.7 2,,478 Antonov An-72.D-36, Series 2A A-F 1, 6, 7 3, 1, 1 An 14,330 lb. t. 0.805 18.9 67.4 125.7 2,478 Antonov An-74.D-36, Series 3A A-F 1, 6, 7 3, 1, 1 An 14,330 lb. t. 0.789 18.9 75.6 146.9 2,491 Antonov An-74.D-36, Series 4A A-F 1, 6, 7 3, 1, 1 An 14,330 lb. t. 0.774 18.9 75.6 146.9 2,491 Antonov An-74TK-300.D-127 AC-S 5, 3 3, 1, 1 An 11,500 shp. 0.397 31.3 24.7 143.9 2,866 Mil Mi-26.D-136 A-S 6, 7 2, 1, 1 An 11,400 shp. 0.437 18.5 54.4 146.3 2,374 Mil Mi-26, Mi-26T.D-436T1 A-F 1, 1, 6, 7 3, 1, 1 An 16,535 lb. t. 0.816 22.9 76.7 150.8 3,197 Tupolev Tu-334.D-436T2 A-F 1, 1, 6, 7 3, 1, 1 An 18,519 lb. t. 0.818 24.4 76.7 150.8 3,351 Tupolev Tu-334-200.D-436T3 A-F 1, 1, 6, 7 3, 1, 1 An 20,724 lb. t. 0.873 29.3 76.7 150.8 3,527 Tupolev Tu-230.D-436TP A-F 1, 1, 6, 7 3, 1, 1 An 16,535 lb. t. 0.37 22.9 76.7 150.8 3,197 Beriev Be-200.D-436-148 A-F 1, 1, 6, 7 3, 1, 1 An 14,110 lb. t. 0.816 19.9 76 150.8 3,087 Antonov An-148.436M A-F 1, 5, 5 3, 1, 1 An 27,377 lb. t. 0.575 26.4 102.3 139.5 5,291 Yakovlev, Ilyushin MS-21.TV3-117VMA-SBM1 A-P 12 2, 2 An 2,500 shp. 0.454 10 47.6 116.3 1,257 Antonov An-140.jakadofSky GmBH, Kottingbrunn, Austria

PJ-W Series Limited 5000 C-S 1 1 An 7 shp. 2.5 1.9 4.5 10 3.5 UAV powerplant Heli Tech Flycam, DLR.PJ-W Series Limited Edition C-S 1 1 An 6.3 shp. 2.6 1.8 4.5 10 3.3 UAV powerplant Heli Tech Flycam, DLR.kaWaSaki Heavy induStrieS, Kobe, Japan

T53-K-13B AC-S 5, 1 2, 2 An 1,400 shp. 0.58 7 23 47.6 540 UH-1H. T53-K-703 AC-S 5, 1 2, 2 An 1,800 eshp. 0.57 8 23 47.6 545 AH-1S, UH-1J.T55-K-712 AC-S 7, 1 2, 2 An 3,750 shp. 0.52 8.2 28.7 48.5 760 CH-47J/JA. klimov, St. Petersburg, Russian Federation

GTD-350 A-S — — — 400 shp. 3.65 — 26.8 53.1 135 Mi-2.RD-33 A-J — — — 18,298 lb. t. — — 40.9 166.5 1,055 Mikoyan MiG-29.TV2-117 A-S — — — 1,500 shp. 2.75 — 29.4 111.9 334 Mi-8.TV3-117 A-S — — — 2,400 shp. 2.15 — 28.7 80.9 295 Mi-14, Mi-24, Ka-27/28/29/31/32/50/52.TV7-117S A-P — — — 3,000 shp. 1.9 — 37 84.1 450 Ilyushin Il-112, Il-114.TV7-117V A-S — — — 2,800 shp. 2.01 — 32.3 78.7 360 Mi-14, Mi-24, Ka-27/28/29/31/32/50/52.VK-800V A-S — — — 800 shp. 2.38 — 23.2 39.4 140 Ansat, Mi-54, Ka-126, Ka-226.VK-1500 A-P — — — 1,500 shp. 2.3 — 33.3 67.5 340 An-38.VK-1500V A-S — — — 1,600 shp. 2.4 — — — 250 Mi-8.VK-2500 A-S — — — 2,700 shp. 2.1 — 28.7 80.9 300 Ka-32, Ka-50, Mi-14, Mi-8MT/Mi-17, Mi-28.liGHt Helicopter turBine enGine co. (lHtec), Madison, AL, USA

CTS800-4N/4K C-S 2 2, 2 An 1,361 shp. 0.47 14.6 23.2 51.1 4081 Super Lynx 300, US-2 Kai. CTS800-5 C-S 2 2, 2 An 1,681 shp. 0.47 14.6 22.3 33.8 340 Intermediate twins.T800-LHT-802 C-S 2 2, 2 An 1,681 shp. 0.47 14.6 22.3 33.8 340 Sikorsky X-2.mitSuBiSHi Heavy induStrieS, Komaki-shi, Aichi-ken, Japan

CT63-M-5A AC-S 6, 1 4 — 317 shp. 0.65 6.2 19 41 139 Hughes 369HS. License production.MG5-110 C-S 1 2 An 876 shp. 0.5 11 29 46.6 340 Mitsubishi MH-2000.MG6-10 C-S 1 1 Ca 70 shp. 0.95 4.5 8 10 — Unmanned helicopter.TJM3 — 1 1 An 441 lb. t. 1.17 5.6 14 34 102 Target drone.TJM4 — 2 2 An 639 lb. t. 1.12 6.7 14 43 123 UAV.TS1-M-10 C-S 1 2 An 940 shp. 0.52 11 24 59 334 OH-1.mtr (itp, mtu aero engines, rolls-royce, turbomeca), Munich, Germany

MTR 390 C-S 2 1, 2 An 1,285 shp. 0.46 13 26.8 42.4 372 Eurocopter Tiger. Growth version in development.MTR 390E C-S 2 1, 2 An 1,465 shp. — 14 26.8 42.4 — Eurocopter Tiger. Growth version in development.



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mtu aero enGineS GmBH., Munich, GermanyRR250-MTU-C20B AC-S 6, 1 2, 2 Ca 420 shp. 0.65 7.2 23.2 40.8 158 BO 105M/P. T64-MTU-7 A-S 14 2, 2 An 3,925 shp. 0.476 13 26 79 712 CH-53G/GS helicopter.T64-MTU-100 A-S 14 2, 2 An 4,330 shp. 0.487 14 26 79 810 CH-53GS helicopter.

npo Saturn, Rybinsk, Russian FederationD-30KP (2) A-F 3, 11 2, 4 Cn 26,667 lb. t. 0.51 19 57.3 — 5,110 Il-76.D-30KP-3 “Burlak” A-F 1, 1, 11 2, 4 Cn 28,890 lb. t. 0.404 17.7 65.5 — 5,717 Il-76.D-30KU A-F 3, 11 2, 4 Cn 24,445 lb. t. 0.498 17.7 57.3 — 5,071 Il-62M.D-30KU-154 A-F 3, 11 2, 4 Cn 23,334 lb. t. 0.498 17 57.3 — 5,082 Tu-154M.

perm enGine co., Perm, Russian FederationPS-90A A-J 1, 2, 13 2, 4 Cn 35,273 lb. t. 0.382 31.32 93.3 195.4 6,498 Il-96, Tu-204, Tu-214.PS-90A-76 A-J 1, 2, 13 2, 4 Cn 35,273 lb. t. 0.382 31.32 93.3 195.4 6,498 Il-76 modifications.poWerjet (Snecma - npo Saturn), Paris, France

SaM146 A-F 1, 3, 6 1, 3 An 17,500 lb. t. 0.37 23.8 48.2 86 3,350 SSJ100.

price induction, Anglet, FranceDGEN P.I. 380 C-F 1, 1 1, 1 An 574 lb. t 0.436 6 22.4 47.5 150 In development. Subject to modifications.DGEN P.I. 390 C-F 1, 1 1, 1 An 740 lb. t 0.452 6 22.4 47.5 150 In development. Subject to modifications.OPUS P.I. 380 C-P 1 1, 1 An 305 shp. 0.75 6 22.4 47.5 — In development. Subject to modifications.

rollS-royce, Dahlewitz, GermanyBR710 A-F 1, 10 2, 2 An 14,000-

17,000 lb. t. 0.639 24 48 134 3,600 Bombardier Global Express/Global 5000,

BR715 A-F 1, 2, 10 2, 3 An 18,500- 21,000 lb. t.

0.637 32 58 147 4,597 Boeing 717-200.

Dart RDa7(Mk522) C-P 2 3 Cn 2,425 shp. 0.58 6.33 38 97.6 1,303 HS748-2B, F27.Dart RDa7(Mk529-8X) C-P 2 3 Cn 2,250 shp. 0.645 5.75 38 97.6 1,257 Gulfstream 1.Dart RDa10(Mk542) C-P 2 3 Cn 3,060 shp. 0.662 6.2 38 99.5 1,397 YS11, Convair.Spey 511-8 A-F 5, 12 2, 2 Cn 11,400 lb. t. 0.82 18.4 32.5 110 2,483 Gulfstream II and III.Spey 555-15 A-F 4, 12 2, 2 Cn 9,900 lb. t. 0.82 15.4 32.5 97 2,257 Fokker 28 Mk. 1/2/3/4000.Spey Mk 202 A-F 5, 12 2, 2 Cn 20,515 lb. t. 0.68 19.5 44 205 4,093 Phantom, Xian JH-7.Spey Mk 250/251 A-F 5, 12 2, 2 Cn 11,995 lb. t. 0.64 19.2 32.5 117 2,740 Nimrod.Spey Mk 512-5W/-14 DW A-F 5, 12 2, 2 Cn 12,550 lb. t. 0.82 21 32.5 110 2,609 BAC 111-475/500.Spey RB. 168-807 A-F 4, 12 2, 2 Cn 11,030 lb. t. 0.66 16.8 32.5 96.7 2,417 Brazilian/Italian AMX.Tay 611 A-F 1, 3, 12 2, 3 Cn 13,850 lb. t. 0.692 15.8 44 95 2,951 Gulfstream IV/IVSP.Tay 611-8C A-F 1, 3, 12 2, 3 Cn 13,850 lb. t. 0.694 15.6 45 95 3,390 Gulfstream G350/G450.Tay 620 A-F 1, 3, 12 2, 3 Cn 13,850 lb. t. 0.692 15.8 44 95 3,185 Fokker 70/100. Tay 650 A-F 1, 3, 12 2, 3 Cn 15,100 lb. t. 0.692 16.2 45 95 3,340 Fokker 100.Tay 651 A-F 1, 3, 12 2, 3 Cn 15,400 lb. t. 0.692 16.6 45 95 3,380 Re-engined Boeing 727-100S.rollS-royce, Derby, UK

RB211-22B A-F 1, 7, 6 1, 1, 3 An 42,000 lb. t. 0.652 24.5 84.83 119.44 9,195 L-1011.RB211-524B4-D A-F 1, 7, 6 1, 1, 3 An 50,000 lb. t. 0.632 28.6 85.8 122.3 9,814 L-1011-250, L-1011-500.RB211-524C2 A-F 1, 7, 6 1, 1, 3 An 51,500 lb. t. 0.652 28.6 84.83 119.44 9,859 747-100/200/300.RB211-524D4-B A-F 1, 7, 6 1, 1, 3 An 53,000 lb. t. 0.632 29.6 85.8 122.34 9,874 747-200/300/SP.RB211-524G A-F 1, 7, 6 1, 1, 3 An 58,000 lb. t. 0.582 32.9 86.3 125.4 9,670 747-400.RB211-524G-T A-F 1, 7, 6 1, 1, 3 An 58,000 lb. t. 0.572 32.9 86.3 125 9,470 747-400.RB211-524H A-F 1, 7, 6 1, 1, 3 An 60,600 lb. t. 0.582 34.5 86.3 125 9,670 747-400, 767-300.RB211-524H-T A-F 1, 7, 6 1, 1, 3 An 60,600 lb. t. 0.572 34.5 86.3 125 9,470 747-400, 767-300.RB211-535C A-F 1, 6, 6 1, 1, 3 An 37,400 lb. t. 0.662 21.1 73.2 118.5 7,294 757-200, 757-200SF.RB211-535E4 A-F 1, 6, 6 1, 1, 3 An 40,100 lb. t. 0.612 25.8 74.1 117.9 7,264 757-200.RB211-535E4B A-F 1, 6, 6 1, 1, 3 An 43,100 lb. t. 0.612 28 74.1 117.9 7,264 757-200/300, 757-200SF, Tupolev Tu-204.Trent 553 A-F 1, 8, 6 1, 1, 5 An 53,000 lb. t. 0.542 34.8 97.4 155 10,660 A340-500.Trent 556 A-F 1, 8, 6 1, 1, 5 An 56,000 lb. t. 0.542 36.3 97.4 155 10,660 A340-600.Trent 600 A-F 1, 8, 6 1, 1, 5 An 63,000 lb. t. 0.542 41 97.4 155 10,660 747-400 developments.Trent 768 A-F 1, 8, 6 1, 1, 4 An 67,500 lb. t. 0.562 33.7 97.4 154 10,550 A330-300.Trent 772B A-F 1, 8, 6 1, 1, 4 An 71,100 lb. t. 0.562 35.5 97.4 154 10,550 A330-200/300/500.Trent 875 A-F 1, 8, 6 1, 1, 5 An 74,600 lb. t. 0.562 34.5 110 172 13,100 777-200.Trent 877 A-F 1, 8, 6 1, 1, 5 An 77,200 lb. t. 0.562 35.9 110 172 13,100 777-200/200ER.



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WORLD MILITARY




Gas Turbine Engines


Trent 884 A-F 1, 8, 6 1, 1, 5 An 84,950 lb. t. 0.562 38.8 110 172 13,100 777-200/200ER/300.Trent 892/892B A-F 1, 8, 6 1, 1, 5 An 91,600 lb. t. 0.56 40.8 110 172 13,100 777-200ER/300. 892B has more altitude capability.Trent 895 A-F 1, 8, 6 1, 1, 5 An 95,000 lb. t. 0.562 41.6 110 172 13,100 777-200ER/300.Trent 970 A-F 1, 8, 6 1, 1, 5 An 70,000 lb. t. 0.522 38.5 116 179 — A380-800.Trent 977 A-F 1, 8, 6 1, 1, 5 An 76,500 lb. t. 0.522 41.1 116 179 — A380F.Trent 1000-A A-F 1, 8, 6 1, 1, 6 An 63,800 lb. t. 0.5062 50 112 160 11,900 787-8, 787-9.Trent 1000-C A-F 1, 8, 6 1, 1, 6 An 69,800 lb. t. 0.5062 50 112 160 11,900 787-8, 787-9.Trent 1000-D A-F 1, 8, 6 1, 1, 6 An 69,800 lb. t. 0.5062 50 112 160 11,900 787-8, 787-9.Trent 1000-E A-F 1, 8, 6 1, 1, 6 An 53,200 lb. t. 0.5062 50 112 160 11,900 787-3, 787-8.Trent 1000-G A-F 1, 8, 6 1, 1, 6 An 67,000 lb. t. 0.5062 50 112 160 11,900 787-8, 787-9.Trent 1000-H A-F 1, 8, 6 1, 1, 6 An 58,000 lb. t. 0.5062 50 112 160 11,900 787-3, 787-8.Trent 1000-J A-F 1, 8, 6 1, 1, 6 An 73,800 lb. t. 0.5062 50 112 160 11,900 787-9.Trent 1000-K A-F 1, 8, 6 1, 1, 6 An 73,800 lb. t. 0.5062 50 112 160 11,900 787-9.Trent XWB A-F — — An 95,000 lb. t. — — 118 — — Airbus A350XWB.rollS-royce, Filton, Bristol, UK

Gem 42 AC-S 4, 1 1, 1, 2 An 1,120 shp. 0.51 13.02 23.5 43.4 404 AgustaWestland Lynx.Gem 1004 AC-S 4, 1 1, 1, 2 An 1,018 shp. 0.53 12.33 23.5 43.1 368 AgustaWestland A129 Mangusta.Gnome H1400 A-S 10 2, 1 An 1,480 shp. 0.61 8.4 22.2 54.8 326 AgustaWestland Sea King.Gnome H1400-1 A-S 10 2, 1 An 1,660 shp. 0.61 9.1 22.2 54.8 326 Boeing Vertol 107, AgustaWestland Sea King.Gnome H1400-1T 7 A-S 10 2, 1 An 1,465 shp 0.63 8.6 22.2 54.8 326 AgustaWestland Sea King.Pegasus 11 A-F 3, 8 2, 2 An 21,500 lb. t. 0.74 14.6 48 137.2 36,205 Harrier, Sea Harrier.Pegasus 11-21 (F402-RR-406A) A-F 3, 8 2, 2 An 22,000 lb. t. 0.74 15.3 48 137.2 39,605 AV-8B, GR. Mk. 5/Mk. 7/Mk. 9, TAV-8B. T Mk10.Pegasus 11-61 (F402-RR-408) A-F 3, 8 2, 2 An 23,800 lb. t. 0.76 16.3 48 137.2 42,605 AV-8B, GR. Mk. 7A/Mk. 9A, T Mk12.Spey Mk 202 A-F 5, 12 2, 2 Cn 20,515 lb. t. A/B 0.68 19.5 44 205 4,093 Phantom, Xian JH-7.Spey Mk 250/251 A-F 5, 12 2, 2 Cn 11,995 lb. t. 0.64 19.2 32.5 117 2,740 Nimrod.Spey RB. 168-807 A-F 4, 12 2, 2 Cn 11,030 lb. t. 0.66 16.8 32.5 96.7 2,417 Brazilian/Italian AMX.Tyne R. Ty 12 Mk 101/515 A-P 6, 9 1, 3 Cn 5,505 eshp. 0.45 13.5 43.2 109 2,219 CL-44, Shorts Belfast.Tyne R. Ty 20 Mk 21/22 A-P 6, 9 1, 3 Cn 6,100 eshp. 0.47 13.97 43.2 109 2,203 Breguet Atlantic, Transall.Tyne R. Ty 20 Mk 801 A-P 6, 9 1, 3 Cn 5,480 eshp. 0.453 13.95 43.2 109 2,187 Aeritalia G.222.Viper 11 A-J 7 1 An 2,500 lb. t. 1.07 4.3 32.9 64 625 Jindivik.Viper 522 A-J 8 1 An 3,360 lb. t. 1 5.6 28.9 92.9 760 HS 125.Viper 531 A-J 8 1 An 3,120 lb. t. 1 5.4 32.9 71.1 790 Soko Jastreb.Viper 535/540 A-J 8 1 An 3,310 lb. t. 1.03 5.5 28 71.1 790 MB-326G, Strikemaster.Viper 601 A-J 8 2 An 3,712 lb. t. 0.95 5.8 28.9 113.9 790 BAe 125-600.Viper 632 A-J 8 2 An 3,960 lb. t. 0.98 5.9 29.4 77.1 830 MB-326, MB-339A/CD.Viper 633 A-J 8 2 An 4,950 lb. t. 1.79 5.9 27.9 174.8 1,219 ORAO/IAR 93 with afterburning.Viper 680 A-J 8 2 An 4,280 lb. t. 1.02 6.8 29 77.3 836 MB-339CB/K.rollS-royce, Indianapolis, IN, USA

501-D22A A-P 14 4 Ca 4,591 shp. 0.54 9.6 44.6 146.3 1,848 L328 commercial Hercules.AE 1107C A-S 14 2, 2 An 6,150 shp. 0.41 16.5 34.2 77.9 973 Bell Boeing V-22.AE 2100A A-P 14 2, 2 An 4,152 shp. 0.46 17 41.5 117 1,578 Saab 2000.AE 2100C A-P 14 2, 2 An 3,271 shp. 0.46 17 41.5 117 1,578 IPTN N-250.AE 2100D2 A-P 14 2, 2 An 4,591 shp. 0.46 17 41.5 117 1,644 Lockheed Martin/Alenia C-27J.AE 2100D3 A-P 14 2, 2 An 4,591 shp. 0.46 17 33.6 124.1 1,644 Lockheed Martin C-130J.AE 2100J A-P 14 2, 2 An 4,591 shp. 0.46 17 33.6 117 — Shinmaywa US-1A.AE 3007A/A1/A1EA3/H A-F 1, 14 2, 3 An 8,917 lb. t. 0.64 23 43.5 106.5 1,581 Embraer ERJ 135/140/145.AE 3007C/C1 A-F 1, 14 2, 3 An 6,764 lb. t. 0.63 23 43.5 106.5 1,572 Citation X.Model 250-B17C AC-P 6, 1 2, 2 Ca 420 shp. 0.66 7.2 22.6 45 198 Aermacchi SF260TP, Maule MT-7-420.Model 250-B17D AC-P 6, 1 2, 2 Ca 420 shp. 0.66 7.2 22.5 45 202 Aermacchi M290TP, Enaer T-35TD, Fuji T-5.Model 250-B17E AC-P 6, 1 2, 2 Ca 420 shp. 0.66 7.2 22.5 45 202 Cessna 402, Nomad N22/24.Model 250-B17F AC-P 6, 1 2, 2 Ca 450 shp. 0.61 7.9 22.6 45 215 B-N Defender 4000, Extra EA-500, Fuji T-7, Grob

G140TP, O&N P210 Silver Eagle, Tradewinds Bonanza.Model 250-C20B/F/J/S/W AC-S 6, 1 2, 2 Ca 420 shp. 0.65 7.2 23.2 38.8 162 Bell 206B/TH-57, Enstrom 480B, RQ-8 Fire Scout,

Schweizer 333.Model 250-C20R AC-S 4, 1 2, 2 Ca 450 shp. 0.61 7.9 23.2 38.8 173 Kamov Ka-226, MDHI MD500E/DN520N, PZL SW-4,

AS355.Model 250-C28B/C C-S 1 2, 2 Ca 500 shp. 0.59 8.4 25.1 47.3 235 Bell 206L-I, BO 105 LS.



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Model 250-C30G/G2 C-S 1 2, 2 Ca 650 shp. 0.59 8.6 25.5 43.2 253 Bell 222, 230.Model 250-C30L/P/R/S/U C-S 1 2, 2 Ca 650 shp. 0.59 8.6 25.1 43.2 252 Bell 206L, OH-58D, MD530F, Soloy AS350 AllStar. Model 250-C30R/1 C-S 1 2, 2 Ca 450 shp. 0.58 8.6 25.1 43.2 173 Bell OH-58D Kiowa Warrior, A109.Model 250-C30R/3 C-S 1 2, 2 Ca 650 shp. 0.59 9.2 25.7 41 274 Bell OH-58D Kiowa Warrior, MH-6 MELB.Model 250-C40B C-S 1 2, 2 Ca 715 shp. 0.57 9.2 25.1 41 280 Bell 430.Model 250-C47B/M C-S 1 2, 2 Ca 650 shp. 0.58 9.2 25.1 41 274 Bell 407, MD 600N.RR300 C-S 1 2, 2 Ca 240-300 shp. 0.67 6.2 25 41 176.5 In development for Robinson, Enstrom, MDH Schweizer.T56-A-14 A-P 14 4 Ca 4,591 shp. 0.54 9.6 49 146.3 1,890 Lockheed P-3C.T56-A-14LFE A-P 14 4 Ca 4,591 shp. 0.54 9.6 49 146.3 1,890 Lockheed CP-140A/B/C.T56-A-15 A-P 14 4 Ca 4,591 shp. 0.54 9.6 44.6 146.3 1,848 Lockheed C-130H.T56-A-15LFE A-P 14 4 Ca 4,591 shp. 0.54 9.6 44.6 146.3 1,848 Lockheed C-130H, C-130H-30.T56-A-16 A-P 14 4 Ca 4,591 shp. 0.54 9.6 44.6 146.3 1,848 Lockheed C-130F/Q/R/T.T56-A-425 A-P 14 4 Ca 4,591 shp. 0.54 9.6 44.6 146.3 1,899 Northrop Grumman C-2A, E-2C.T56-A-427 A-P 14 4 Ca 5,823 shp. 0.47 12 48.3 146.1 1,940 Northrop Grumman E-2C+.T63-A-720 AC-S 6, 1 2, 2 Ca 420 shp. 0.65 7.3 23.2 40.8 158 Bell OH-58C, TH57.T703-A-700 C-S 1 2, 2 Ca 650 shp. 0.58 8.6 25.1 43.2 255 Bell OH-58D.TF41-A-400/A-2B A-F 3, 2, 11 2, 2 Cn 15,000 lb. t. 0.67 21.4 39.5 114.2 3,204 A-7E, A-7H (Hellenic AF).rollS-royce, allison advanced development co., Indianapolis, IN, USA

J104-AD-100 C-J 1 1 An 485 lb. t. 1.24 — 11.6 19.5 41 Missiles, targets, UAVs.Model 120 C-J 1 1 An 229 lb. t. 1.27 — 8 16 23 Missiles, targets, UAVs.rollS-royce, Snecma, mtu aero engines, UK, France and Germany

Tyne R. Ty 20 Mk. 21/22 A-P 6, 9 1, 3 Ca 6,100 eshp. 0.47 13.7 55 109 2,436 Atlantique, Atlantique new generation, Transall.

rollS-royce turBomeca ltd., UK and FranceAdour Mk. 811/815 A-F 2, 5 1, 1 An 8,400 lb. t. A/B 0.78 11.3 30.8 114 1,633 Jaguar International.Adour Mk. 861 A-F 2, 5 1, 1 An 5,710 lb. t. 0.74 11.3 30 77 1,282 Hawk.Adour Mk. 871 (F405-RR-401) A-F 2, 5 1, 1 An 5,845 lb. t. 0.78 11.3 30.9 76.7 1,306 Hawk 100/200, T-45.RTM 322-01/8 AC-S 3, 1 2, 2 An 2,101 shp. 0.45 14 25.9 46.1 558 EH101, Merlin Mk. 1.RTM 322-01/9 AC-S 3, 1 2, 2 An 2,412 shp. 0.42 16 25.9 46.1 502 NH90.RTM 322-01/9A AC-S 3, 2 2, 3 An 2,544 shp. 0.42 16 25.9 46.1 502 NH90.RTM 322-01/12 AC-S 3, 1 2, 2 An 2,101 shp. 0.45 14 25.9 46.1 558 WAH-64.RTM 322-02/8/Mk. 250 AC-S 3, 1 2, 2 An 2,270 shp. 0.45 14 25.9 46.1 564 EH101, Merlin HC Mk. 3.Safran Group - microturbo, Toulouse, France

TRI 40 A-J 4 1 An 760 lb. t. 1.18 6.2 11 28 93 NSM missile, Exocet block 3.TRI 60-1 A-J 3 1 An 787 lb. t. 1.18 3.7 13 42 116 Sea Eagle missile.TRI 60-2 A-J 3 1 An 830 lb. t. 1.26 3.8 13 44.8 114 RBS 15 missile, MQM 107B.TRI 60-3 A-J 3 1 An 900 lb. t. 1.28 3.9 13 53.2 150 C22 drone.TRI 60-5 A-J 3 1 An 995 lb. t. 1.27 4.1 13 57 134 MQM-107D/E, Skua, Lakshya, BQM 167 target

drone, Sky-X UAV, Carapas UAV, Mirach 150 UAV.TRI 60-30 A-J 4 1 An 1,280 lb. t. 1.11 6.4 14.3 42.3 144 Apache A, Scalp EG, Storm Shadow missiles.TRS 18 C-J 1 1 An 360 lb. t. 1.26 4.7 12 40.7 97 Mirach 100/5 drone.Safran Group - Snecma, Paris, France

Atar 9K50 A-J 9 2 An 16,000 lb. t. A/B 1.96 6.15 40.5 232 34,884 Dassault Mirage F1, Mirage 50.M53-5 A-F 3, 5 2 An 19,850 lb. t. A/B 2.05 9 41.5 199.64 32,404 Dassault Mirage 2000.M53-P2 A-F 3, 5 2 An 21,400 lb. t. A/B 2.07 9.8 41.5 199.64 33,004 Dassault Mirage 2000, 2000-5, 2000-9.M88-2 A-F 3, 6 1, 1 An 17,000 lb. t. A/B 1.72 24.5 30.3 143.14 19,204 Rafale B/C/M, light combat planes, trainers.Larzac 04-C6 A-F 2, 4 1, 1 An 2,980 lb. t. 0.71 10.7 23.7 46.4 640 Dassault-Breguet/Dornier Alpha Jet.Larzac 04-C20 A-F 2, 4 1, 1 An 3,170 lb. t. 0.74 11.1 23.7 46.4 666 Dassault-Breguet/Dornier Alpha Jet, MiG-AT.Larzac 04-H20 A-F 2, 4 1, 1 An 3,200 lb. t. 0.76 11.1 23.7 46.4 — Hindustan Aeronautics HJT36.Larzac 04-R20 A-F 2, 4 1, 1 An 3,200 lb. t. 0.76 11.1 23.7 46.4 — MiG-AT.Safran Group - turbomeca, Bordes, France

Arbizon 3B2 AC-J 1, 1 1 An 907 lb. t. 1.12 5.85 16.1 53.6 253 Matra BAE Otomat missiles.Arbizon 3D AC-J 1, 1 1 An 936 lb. t. 1.08 5.85 17 54.2 253 Alenia Matra Milas missiles.Arriel 1B AC-S 1, 1 2, 1 An 641 shp. 0.595 8 23.5 47.7 252 Eurocopter AS350BA.Arriel 1C1 AC-S 1, 1 2, 1 An 724 shp. 0.58 8 24.7 47.2 262 Eurocopter SA365N1.Arriel 1C2 AC-S 1, 1 2, 1 An 738 shp. 0.574 8 24 45.9 262 Eurocopter AS365N2.Arriel 1D1 AC-S 1, 1 2, 1 An 732 shp. 0.579 8 24.1 47.2 269 Eurocopter AS350B1/B2.



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WORLD MILITARY




Gas Turbine Engines


Arriel 1E2 AC-S 1, 1 2, 1 An 738 shp. 0.574 8 27.3 46.7 276 Eurocopter BK117C1.Arriel 1K1 AC-S 1, 1 2, 1 An 738 shp. 0.574 8 24.3 47.2 271 Agusta A109K/K2.Arriel 1M/1M1 AC-S 1, 1 2, 1 An 773/783 shp. 0.569 8 24.7 47.2 271 Eurocopter AS565.Arriel 1S1 AC-S 1, 1 2, 1 An 723 shp. 0.567 8 31 60.6 287 Sikorsky S-76A+, S-76C.Arriel 2B/2B1 AC-S 1, 1 1, 1 An 848 shp. 0.548 8 24.3 46.5 282 Eurocopter AS350B3/EC130.Arriel 2C AC-S 1, 1 1, 1 An 839 shp. 0.548 8 24.3 46.5 282 Eurocopter AS365N3.Arriel 2C1 AC-S 1, 1 1, 1 An 848 shp. 0.548 8 22.7 40 282 Eurocopter EC155B.Arriel 2C2 AC-S 1, 1 1, 1 An 944 shp. 0.545 8 22.7 39.9 282 Eurocopter EC155.Arriel 2S1 AC-S 1, 1 1, 1 An 856 shp. 0.54 8 28.1 60.6 282 Sikorsky S-76C+.Arriel 2S2 AC-S 1, 1 1, 1 An 923 shp. 0.54 8 28.1 60.6 282 Sikorsky S-76C++.Arrius 1A C-S 1 1, 1 An 479 shp. 0.555 8.2 23.1 45.6 251 Eurocopter AS355N.Arrius 1M C-S 1 1, 1 An 479 shp. 0.555 8.2 23.1 45.6 251 Eurocopter AS555N.Arrius 2B1/2B1A-1 C-S 1 1, 1 An 670 shp. 0.526 9 27.2 46.6 251 Eurocopter EC135.Arrius 2B2 C-S 1 1, 1 An 633 shp. 0.539 8.4 27.2 46.6 251 Eurocopter EC135.Arrius 2F C-S 1 1, 1 An 504 shp. 0.55 8.5 26.5 53.2 227 Eurocopter EC120.Arrius 2K1 C-S 1 1, 1 An 750 shp. 0.526 9 25.1 38.3 254 Agusta A109 Power.Arrius 2K2 C-S 1 1, 1 An 716 shp. 0.527 9 25.1 38.3 254 Agusta A109 LUH.Artouste 3B AC-S 1, 1 3 An 592 shp. 0.744 5.35 26.2 71.4 400 Eurocopter SA315, SA316.Astazou 3 AC-S 1, 1 3 An 592 shp. 0.644 5.7 20 56.4 324 Eurocopter SA341.Astazou 14 AC-S 2, 1 3 An 592 shp. 0.634 7.5 22.2 57.9 348 Eurocopter SA319, SA342.Astazou 16D AC-P 2, 1 3 An 969 shp. 0.525 8 22.9 61.2 452 Jetstream.Astazou 16G AC-P 2, 1 3 An 1,021 shp. 0.525 8 25.4 61.2 503 Pucara.Makila 1A1 AC-S 3, 1 2, 2 An 1,820 shp. 0.484 10.4 26.8 82.8 518 Eurocopter AS332, SA330.Makila 1A2/1K2 AC-S 3, 1 2, 2 An 1,845 shp. 0.476 10.4 26.5 83.3 518 Eurocopter AS532/Denel Rooivalk.Makila 2A AC-S 3, 1 2, 2 An 2,101 shp. 0.469 11 30.9 83.3 615 Eurocopter EC225, EC725.TM 333 2B2 AC-S 2, 1 1, 1 An 1,106 shp. 0.517 10.5 29.7 41.1 367 HAL Dhruv.Turmo 3C7 AC-S 1, 1 2, 2 An 1,610 shp. 0.632 5.9 28.3 78 660 Eurocopter SA321, free turbine.Turmo 4C AC-S 1, 1 2, 1 An 1,560 shp. 0.632 5.9 28.3 85.5 515 Eurocopter SA330, free turbine.tecHnical directionS inc., Ortonville, MI, USA

TDI-J5 C-J 1 1 An 55 lb. t. 1.4 4 5 7.3 6.3 Missiles, decoys, targets, UAVs.TDI-J7 C-J 1 1 An 100 lb. t. 1.5 3.8 7 9.2 12 Missiles, decoys, targets, UAVs.TDI-J45 C-J 1 1 An 30 lb. t. 1.3 4.2 4.5 7.3 6.1 Locaas, NLOS-LS LAM.teledyne continental motorS-turBine enGineS, Toledo, OH, USA

F408-CA-400 AC-F 1, 1 1 An 1,000 lb. t. 0.97 8.5 13.2 37 145 UAV-MR (BQM-145A).J69-T-25A C-J 1 1 An 1,025 lb. t. 1.14 3.9 22.3 35.4 358 Cessna T-37B.J69-T-41B AC-J 1, 1 1 An 1,920 lb. t. 1.1 5.5 22.3 45 350 Northrop Grumman BQM-34A target.J69-T-406 AC-J 1, 1 1 An 1,920 lb. t. 1.11 5.5 22.5 45 360 Northrop Grumman BQM-34E/F supersonic target.J402-CA-100 AC-J 1, 1 1 An — — — 12.4 35.3 107 Lockheed Martin Jassm.J402-CA-400 AC-J 1, 1 1 An 660 lb. t. 1.2 5.6 12.5 29 102 Boeing Harpoon, SLAM, SLAM-ER missiles.J402-CA-700 AC-J 1, 1 1 An 640 lb. t. 1.2 5.5 12.5 29 113 RPVs, targets.J402-CA-702 AC-J 2, 1 1 An 960 lb. t. 1.03 8.5 12.5 33 138 MQM-107.J700-CA-400 C-J 1 1 An 177 lb. t. 1.21 5.7 8.5 14.8 39 ITALD (ADM-141C).turBo-union ltd. (avio, rolls-royce, mtu aero engines), Bristol, UK

RB199 Mk. 103 A-F 3, 3, 6 1, 1, 2 An 16,000 lb. t. A/B 0.65 23.5 34 128 1,549 Panavia Tornado IDS.RB199 Mk. 104 A-F 3, 3, 6 1, 1, 2 An 16,400 lb. t. A/B 0.65 23.5 34 142 1,549 Panavia Tornado ADV.RB199 Mk. 105 A-F 3, 3, 6 1, 1, 2 An 16,800 lb. t. A/B 0.65 24.5 34 130 1,611 Panavia Tornado ECR.united tecHnoloGieS corp., pratt & Whitney canada inc., Longueuil, Quebec, Canada

JT15D-5/5A AC-F 1, 1, 1 1, 2 An 2,965 lb. t./ 2,900 lb. t.

0.551 12.6 27.3 60.4 632 Beechjet 400A, Cessna Citation Navy Trainer T-47A, Cessna T-47A, Cessna Citation V.

JT15D-5B AC-F 1, 1, 1 1, 2 An 2,900 lb. t. 0.551 — 27 60.4 635 Beech T-1A. JT15D-5C AC-F 1, 1, 1 1, 2 An 3,190 lb. t. 0.573 13.5 28 61 666 Agusta S211/S211A.JT15D-5D AC-F 1, 1, 1 1, 2 An 3,045 lb. t. 0.56 13.1 27 61 627 Cessna Citation Ultra, Cessna UC-35A/B.PT6A-21 AC-P 3, 1 1, 1 An 550 shp. 0.63 — 19 62 327 Turbine Air Bonanza, Beech King Air C90A/B/SE.PT6A-25 AC-P 3, 1 1, 1 An 550 shp. 0.63 — 19 62 353 Beech T-34C.PT6A-25C AC-P 3, 1 1, 1 An 750 shp. 0.595 — 19 62 338 Embraer EMB-312 Tucano, Pilatus Turbo Trainer PC-7/

Mk. II; PZL-Okezie PZL-130 TC-II Turbo-Orlik.PT6A-42 AC-P 3, 1 1, 2 An 850 shp. 0.601 8 19 66.9 403 Beech King Air 200/B200, Beech C12F.



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PT6A-60A AC-P 4, 1 1, 2 An 1,050 shp. 0.548 8.5 19 72.5 475 Super Beech King Air 300/350.PT6A-64 AC-P 4, 1 1, 2 An 700 shp. 0.703 8.5 19 70 456 Socata TBM 700.PT6A-65B AC-P 4, 1 1, 2 An 1,100 shp. 0.536 — 19 74 481 Ayres TurboThrush Commander A2RT-65; PZL Mielec

M28 Skytruck, Raytheon Beech 1900/1900C-1.PT6A-66 AC-P 4, 1 1, 2 An 850 shp. 0.62 9.5 19 70 456 Piaggio Avanti P.180.PT6A-67B AC-P 4, 1 1, 2 An 1,200 shp. 0.546 10.8 19 74 530 Pilatus PC-12.PT6A-67D AC-P 4, 1 1, 2 An 1,271 shp. 0.546 10.8 19 74 515 Beech 1900D.PT6A-68 AC-P 4, 1 1, 2 An 1,250 shp. 0.54 — 19 72.2 572 T-6A Texan II.PT6A-68B AC-P 4, 1 1, 2 An 1,600 shp. 0.54 — 19 72.2 575 Pilatus PC-21.PT6A-114/114A AC-P 3, 1 1, 1 An 600/675 shp. 0.64 — 19 62 350 Cessna 208/208B Caravan I.PT6A-135A AC-P 3, 1 1, 1 An 750 shp. 0.585 7 19 62 338 Cessna Conquest I, Piper Cheyenne I, Beech King Air F90-1.PT6B-37A AC-S 3, 1 1, 1 An 900 shp. 0.584 — 19.5 64.4 385 Agusta A119 Koala.PT6C-67A AC-S 4, 1 1, 1 An 1,940 shp. 0.47 — 22.5 59.3 — Bell/Agusta BA609.PT6C-67C AC-S 4, 1 1, 2 An 1,100 shp. 0.49 — 22.5 59.3 — Agusta Bell AW139.PT6T-3B/BF AC-S 3, 1 1, 1 An 1,800 shp. 0.6 — 43.5 65.8 668 Agusta Bell 412, 412SP, 412 HP, 412 EP.PT6T-3D/DF AC-S 3, 1 1, 1 An 1,800 shp. 0.595 — 43.5 65.8 692/681 Agusta Bell 412, 412SP, 412 HP, 412 EP.PT6T-6 AC-S 3, 1 1, 1 An 1,875 shp. 0.591 — 43.5 65.8 660 Agusta Bell 212, 412/SP/HP/EP, Sikorsky S58T.PT6T-68 AC-S 3, 1 1, 1 An 1,970 shp. 0.591 — 43.5 65.8 665 Bell/Agusta 412HP.PW118/118A C-P 2 1, 1, 2 An 1,800 shp. 0.504 11.4 25 81 861 Embraer EMB-120.PW120 C-P 2 1, 1, 2 An 2,000 shp. 0.485 11.4 31 84 921 ATR 42-300/320.PW121 C-P 2 1, 1, 2 An 2,150 shp. 0.477 11.8 25 84 936 ATR 42-400/500, Bombardier Q100.PW121A C-P 2 1, 1, 2 An 2,200 shp. 0.474 12 31 84 — ATR 42-400/500.PW123/123E C-P 2 1, 1, 2 An 2,380 shp. 0.47 13.9 26 84 992 Bombardier Q300.PW123B C-P 2 1, 1, 2 An 2,500 shp. 0.463 13.9 33 84 992 Bombardier Q300.PW123C/D C-P 2 1, 1, 2 An 2,150 shp. 0.483 13.9 33 84 992 Bombardier Q200.PW124B C-P 2 1, 1, 2 An 2,400 shp. 0.468 13.9 25 84 — ATR 72-200.PW127 C-P 2 1, 1, 2 An 2,750 shp. 0.459 14.7 33 84 — ATR 72-210.PW127B/C/D/F C-P 2 1, 1, 2 An 2,750 shp. 0.459 14.7 26 84 1,060 Fokker 60 Utility, ATR 72. PW127E C-P 2 1, 1, 2 An 2,400 shp. 0.474 14.7 26 84 1,060 ATR 42-400/500.PW127G C-P 2 1, 1, 2 An 2,920 shp. 0.453 — 26 84 1,067 CASA C-295.PW150A AC-P 3, 1 1, 1, 2 An 5,071 shp. 0.433 18 30.2 95.4 1,583 Bombardier Q400.PW206B/B2 C-S 1 1, 1 An 431 shp. 0.553 — 19.7 41 247/261 Eurocopter EC135.PW206C C-S 1 1, 1 An 561 shp. 0.542 — 19.7 35.9 237 Agusta A109E.PW206E C-S 1 1, 1 An 646 shp. — — 22.3 37.7 — MD Explorer.PW207C C-S 1 1, 1 An 650 shp. — — 22.3 35.9 — Agusta A109 Grand.PW207D C-S 1 1, 1 An 572 shp. 0.537 — 19.7 35.9 243 Bell 427.PW207E C-S 1 1, 1 An 646 shp. 0.54 — 19.7 37.7 240 MD Helicopter. PW207K C-S 1 1, 1 An 646 shp. — — 19.7 35.9 238 Kazan Ansat.PW305A AC-F 1, 5 2, 3 An 4,679 lb. t. 0.388 19 34.3 65 993 Learjet 60.PW305B AC-F 1, 5 2, 3 An 5,266 lb. t 0.391 19 44 82 993 Hawker 1000.PW306A AC-F 1, 5 2, 3 An 6,040 lb. t. 0.394 — 36.5 75.7 1,139 Gulfstream G200.PW306B AC-F 1, 5 2, 3 An 6,050 lb. t. 0.421 — 36.5 75.7 1,142 Fairchild Dornier 328JET.PW306C AC-F 1, 5 2, 3 An 5,770 lb. t. — — 36.5 75.7 1,150 Cessna Citation Sovereign.PW308A AC-F 1, 5 2, 3 An 6,904 lb. t. 0.415 — 39 93 1,344 Hawker 4000.PW308C AC-F 1, 5 2, 3 An 7,002 lb. t. 0.416 25.5 39 93 1,354 Dassault Falcon 2000EX.PW530A AC-F 1, 3 1, 2 An 2,887 lb. t. 0.475 — 27.6 60 617 Cessna Citation Bravo.PW535A AC-F 1, 1, 3 1, 2 An 3,400 lb. t. — — 28.15 63.9 699 Cessna Citation Ultra Encore.PW545A AC-F 1, 1, 3 1, 3 An 3,804 lb. t. 0.436 — 32 68 805 Cessna Citation Excel.PW545B — — — — 3,991 lb. t. — — — — — Cessna Citation XLS.PW610F — — — — 900 shp. — — 18.7 41.7 — Eclipse 500 Jet.PW615F — — — — 1,350 shp. — — 21.9 49.3 — Citation Mustang.PW617F — — — — 1,615 shp. — — — — — Embraer VLJ.united tecHnoloGieS corp., pratt & Whitney large commercial engines, East Hartford, CT, USA

JT8D-15 A-F 2, 4, 7 1, 3 Cn 15,500 lb. t. 0.63 16.6 39.9 120 3,414 727, 737, DC-9.JT8D-15A A-F 2, 4, 7 1, 3 Cn 15,500 lb. t. 0.599 16.4 39.9 120 3,474 727, 737, DC-9.



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WORLD MILITARY




Gas Turbine Engines


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JT8D-17 A-F 2, 4, 7 1, 3 Cn 16,000 lb. t. 0.645 16.9 39.9 120 3,430 727, 737, DC-9-30/50.JT8D-17A A-F 2, 4, 7 1, 3 Cn 16,000 lb. t. 0.613 16.9 39.9 120 3,475 727, 737, DC-9-30/50.JT8D-17AR A-F 2, 4, 7 1, 3 Cn 17,400 lb. t. 0.622 18.5 39.9 120 3,600 727JT8D-17R A-F 2, 4, 7 1, 3 Cn 17,400 lb. t. 0.655 18.2 39.9 120 3,495 727JT8D-209 A-F 1, 6, 7 1, 3 Cn 19,250 lb. t. 0.501 17.4 49.2 154.1 4,435 MD-80 series.JT8D-217/217A A-F 1, 6, 7 1, 3 Cn 20,850 lb. t. 0.51 18.6 49.2 154.1 4,470 MD-80 series.JT8D-217C A-F 1, 6, 7 1, 3 Cn 20,850 lb. t. 0.5 21 49.2 154.1 4,515 MD-80 series.JT8D-219 A-F 1, 6, 7 1, 3 Cn 21,700 lb. t. 0.519 21 49.2 154.1 4,515 MD-80 series, US Air Force E-8 re-engining. JT9D-7A A-F 1, 3, 11 2, 4 An 46,250 lb. t. 0.364 22.5 95.6 128.2 8,850 747, 747SP/SR.JT9D-7F A-F 1, 3, 11 2, 4 An 48,000 lb. t. 0.367 22.8 95.6 128.2 8,860 747, 747SP/SR.JT9D-7J A-F 1, 3, 11 2, 4 An 50,000 lb. t. 0.37 23.5 95.6 128.2 8,860 747, 747SP/SR.JT9D-7Q/Q3 A-F 1, 3, 11 2, 4 An 53,000 lb. t. 0.375 24.5 97 132.2 9,295 747-200B/C/F.JT9D-7R4D/D1 A-F 1, 4, 11 2, 4 An 48,000 lb. t. 0.34 23.4 97 132.7 8,905 D for 767-200; D1 for A310.JT9D-7R4E/E1 A-F 1, 4, 11 2, 4 An 50,000 lb. t. 0.343 24.2 97 132.7 8,905 E for 767-200; E1 for A310.JT9D-7R4E3/E4 A-F 1, 4, 11 2, 4 An 50,000 lb. t. 0.346 24.2 97 132.7 8,905 767, A310.JT9D-7R4G2 A-F 1, 4, 11 2, 4 An 54,750 lb. t. 0.36 26.3 97 132.7 8,140 747-300.JT9D-7R4H1 A-F 1, 4, 11 2, 4 An 56,000 lb. t. 0.364 26.7 97 132.7 8,885 A300-600.PW2037 A-F 1, 4, 12 2, 5 An 38,250 lb. t. 0.342 27 84.8 146.8 7,300 757.PW2040 A-F 1, 4, 12 2, 5 An 41,700 lb. t. 0.352 28 84.8 146.8 7,300 757, C-17.PW2043 A-F 1, 4, 12 2, 5 An 43,000 lb. t. 0.362 31.9 84.8 146.8 7,300 757.PW4050 A-F 1, 4, 11 2, 4 An 50,000 lb. t. 0.348 26.3 97 132.7 9,213 767-200/200ER/300.PW4052 A-F 1, 4, 11 2, 4 An 52,200 lb. t. 0.351 27.5 97 132.7 9,213 767-200ER, 767-200.PW4056 A-F 1, 4, 11 2, 4 An 56,750 lb. t. 0.359 29.7 97 132.7 9,213 767-300/300ER, 747-400.PW4060 A-F 1, 4, 11 2, 4 An 60,000 lb. t. 0.365 31.2 97 132.7 9,213 767-300ER/400, 747-400.PW4062 A-F 1, 4, 11 2, 4 An 62,000 lb. t. 0.365 32.3 97 132.7 9,213 767-300ER.PW4084 A-F 1, 6, 11 2, 7 An 86,760 lb. t. 0.334 34.4 118.5 191.6 14,920 777.PW4090 A-F 1, 6, 11 2, 7 An 91,790 lb. t. 0.355 38.6 118.5 191.6 15,585 777.PW4152 A-F 1, 4, 11 2, 4 An 52,000 lb. t. 0.339 27.1 97 132.7 9,332 A310-300.PW4156A A-F 1, 4, 11 2, 4 An 56,000 lb. t. 0.35 29.7 97 132.7 9,332 A310-300.PW4158 A-F 1, 4, 11 2, 4 An 58,000 lb. t. 0.355 32 132.7 132.7 9,332 A300-600R.PW4164 A-F 1, 5, 11 2, 5 An 64,000 lb. t. 0.35 32 106.9 163 12,178 A330.PW4168A A-F 1, 5, 11 2, 5 An 68,600 lb. t. 0.348 31.8 106.9 163 12,178 A330.PW4460 A-F 1, 4, 11 2, 4 An 60,000 lb. t. 0.371 31.2 97 132.7 9,332 MD-11.PW4462 A-F 1, 4, 11 2, 4 An 62,000 lb. t. 0.378 32.3 97 137.2 9,332 MD-11.PW6122A A-F 1, 4, 6 1, 3 An 22,100 lb. t. 0.36 25.7 56.5 108.2 5,040 A318.PW6124A A-F 1, 4, 6 1, 3 An 23,800 lb. t. 0.37 27.9 56.5 108.2 5,040 A318.

united tecHnoloGieS corp., pratt & Whitney military engines, East Hartford, CT, USAF100-PW-100 A-F 3, 10 2, 2 An 22,600 lb. t. A/B 2.1 24.5 46.5 191.2 3,149 F-15A/B/C/D. Production ended.F100-PW-200 A-F 3, 10 2, 2 An 22,600 lb. t. A/B 2.1 24.5 46.5 191.2 3,190 F-16A/B/C/D. Production ended.F100-PW-220 A-F 3, 10 2, 2 An 23,770 lb. t. A/B 2.1 25 46.5 191.2 3,265 F-15C/D/E, F-16A/B/C/D.F100-PW-220E A-F 3, 10 2, 2 An 23,770 lb. t. A/B 2.1 25 46.5 191.2 3,245 Upgrade for F100-PW-100/200. F-15C/D,F-16A/B/C/D. F100-PW-229 A-F 3, 10 2, 2 An 29,100 lb. t. A/B 1.94 32.4 46.5 191.2 3,795 F-15E/I/S, F-16C/D. Increased performance.F100-PW-232 A-F 3, 10 2, 2 An 32,500 lb. t. 1.91 35 46.5 190.7 4,065 F100-229 performance and durability upgrade.F117-PW-100 A-F 1, 4, 12 2, 5 An 40,900 lb. t. 0.34 27.6 84.5 146.8 7,100 Boeing C-17. MTU is a partner.F119-PW-100 A-F 3, 6 1, 1 An 35,000 lb. t. — — — — — Lockheed Martin F-22.F135-PW-100 A-F 3, 6 1, 2 An 40,000 lb. t. — — — — — Lockheed Martin land-based CTOL F-35A.F135-PW-400 A-F 3, 6 1, 2 An 40,000 lb. t. — — — — — Lockheed Martin naval CTOL F-35C.F135-PW-600 A-F/S 3, 6 1, 2 An 40,000 lb. t. — — — — — Lockheed Martin Stovl F-35B. Clutch/shaft to lift fan.J52-P-8A/B/C A-J 12 2 Cn 9,300 lb. t. 0.86 13.6 32 117 2,129 Boeing A-4.J52-P-408 A-J 12 2 Cn 11,200 lb. t. 0.89 14.6 32 119 2,318 Boeing A-4, Northrop Grumman/US Navy EA-6B.J58 A-J 9 2 Cn 34,500 lb. t. 2.174 8.8 55.4 211.7 6,326 Lockheed SR-71, with A/B. Partial ramjet cruise.TF30-P-3/P-103 A-F 3, 6, 7 1, 3 Cn 18,500 lb. t. 2.5 17.1 49 242 4,079 F-111C.TF30-P-108 A-F 3, 6, 7 1, 3 Cn 20,350 lb. t. 2.7 16.5 51 242 4,166 F-111G.TF30-P-109RA A-F 3, 6, 7 1, 3 Cn 20,240 lb. t. 2.62 18.1 49 242 4,106 F-111C.TF30-P-414/414A A-F 3, 6, 7 1, 3 Cn 20,900 lb. t. 2.78 19.8 51 236 4,251 Northrop Grumman F-14A.TF33-P-3 A-F 2, 6, 7 1, 3 Cn 17,000 lb. t. 0.52 13 53 136 3,900 Boeing B-52H.TF33-P-5/-P-105 A-F 2, 6, 7 1, 3 Cn 18,000 lb. t. 0.515 13.5 53 137.4 4,275 Boeing C-135, RC-135, TC-135, WC-135.TF33-P-7/7A A-F 2, 7, 7 1, 3 Cn 21,000 lb. t. 0.56 15.6 54 142 4,650 Lockheed C-141.TF33-P-9 A-F 2, 6, 7 1, 3 Cn 18,000 lb. t. 0.515 13.5 53.1 137.4 4,340 Boeing EC-135, RC-135.TF33-PW-100A A-F 2, 7, 7 1, 3 Cn 21,000 lb. t. 0.56 15.6 54 142 4,790 Boeing E-3A.TF33-PW-102/102A A-F 2, 6, 7 1, 3 Cn 18,000 lb. t. 0.54 13.6 53 137 4,340 Boeing C-18A, C/KC-135E, E-8C.



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TF33-PW-102B A-F 2, 6, 7 1, 3 Cn 18,000 lb. t. 0.515 13.56 53.1 136.3 4,340 Northrop Grumman E-8C.TF33-PW-102C A-F 2, 6, 7 1, 3 Cn 19,000 lb. t. 0.525 13.56 53.1 136.3 4,340 Northrop Grumman E-8C.TF33-PW-103 A-F 2, 6, 7 1, 3 Cn 17,000 lb. t. 0.505 13.4 53.1 136.3 3,900 Boeing B-52H.volvo aero corp., Trollhattan, Sweden

RM12 A-F 3, 7 1, 1 An 18,100 lb. t. 1.78 27.5 34.8 159 2,325 Version of GE F404 for JAS 39 Gripen.Walter enGineS a.S., Prague, Czech Republic

M601D AC-P 2, 1 1, 1 An 724 shp. 0.65 6.55 25.6 64.96 426 Let L-410UVP commuter.M601D-1 AC-P 2, 1 1, 1 An 724 shp. 0.65 6.55 25.6 64.96 426 PZL-106 BT Turbo Kruk, Thrush S2R.M601D-2 AC-P 2, 1 1, 1 An 504 shp. 0.69 6.03 25.6 64.96 426 Dornier Do-28, SMG-92 Turbo Finist.M601D-11 AC-P 2, 1 1, 1 An 604 shp. 0.69 6.12 25.6 64.96 426 FU-24 Fletcher (M601D-11NZ), AT-300, Cessna 207.M601E AC-P 2, 1 1, 1 An 751 shp. 0.65 6.9 25.6 64.96 441 Let L-410UVP-E, SM-92T Finist.M601E-11 AC-P 2, 1 1, 1 An 751 shp. 0.65 6.9 25.6 64.96 441 AT-300 to AT-502, Cessna Caravan, DHC-3 Otter,

Schweizer Ag-Cat, Thrush S2R. M601E-11A AC-P 2, 1 1, 1 An 705 shp. 0.65 6.41 25.6 64.96 441 Beech King Air 90 and A100, Lancair IV Turbine,

Piper PA-31 Navajo.M601E-21 AC-P 2, 1 1, 1 An 751 shp. 0.65 6.9 25.6 64.96 441 Let L-410UVP-E, hot and high version.M601F AC-P 2, 1 1, 1 An 777 shp. 0.63 6.9 25.6 64.96 445 Let L-420, Vulcanair VF-600W, SM-92TF Finist,

Sokol M101T.M601T AC-P 2, 1 1, 1 An 751 shp. 0.65 7 25.6 64.96 445 PZL-130TM.M601Z AC-P 2, 1 1, 1 An 544 shp. 0.78 6.55 25.6 64.96 441 Zlin Z-137T. WilliamS international, Walled Lake, MI, USA

F107-WR-101 AC-F 4, 1 1, 2 An 600 lb. t. — 13.8 12 48.5 146 Boeing ALCM.F107-WR-105 A-F 4, 1 1, 2 An 750 lb. t. — — 12 38.25 — Lockheed Martin Jassm-ER missile.F107-WR-402 AC-F 4, 1 1, 2 An 700 lb. t. — — 12 36.9 — Boeing/Raytheon Tomahawk.F112-WR-100 A-F 4, 1 1, 2 An — — — — — — Advanced cruise missiles.F121-WR-100 A-F 1, 6 2 An 150 lb. t. — — 8.3 26 42 Missile applications.F122-WR-100 A-F 2, 5 2 An 1,000 lb. t. — — 13.5 — — Missiles.F415-WR-400 A-F 2, 5 2 An 700 lb. t. — — 9.5 32 — Raytheon Tactical Tomahawk cruise missile.FJ33-4A AC-F 1, 3, 1 1, 2 An 1,500 lb. t. — — 17.5 38.5 — Adam A700, Diamond D-Jet, Excel SportJet,

Spectrum 33, Epic Elite and Victory.FJ33-4A-19 AC-F 1, 3, 1 1, 2 An 1,900 lb. t. — — 17.5 38.5 — ATG Javelin, Cirrus Jet.FJ44-1A AC-F 1, 1, 1 1, 2 An 1,900 lb. t. 0.456 — 20.9 40.2 445 Cessna Citation CJ1.FJ44-1AP AC-F 1, 1, 1 1, 2 An 2,100 lb. t. — — 20.9 40.2 — Cessna Citation CJ1+.FJ44-1C AC-F 1, 1, 1 1, 2 An 1,500 lb. t. 0.46 — 20.9 40.2 445 Saab SK60.FJ44-2A AC-F 1, 3, 1 1, 2 An 2,300 lb. t. — — 21.8 47.2 — Sino-Swearingen SJ30-2. FJ44-2C AC-F 1, 3, 1 1, 2 An 2,400 lb. t. — — 21.8 47.2 — Cessna Citation CJ2.FJ44-3A AC-F 1, 3, 1 1, 2 An 3,000 lb. t. — — 23 48 — Cessna Citation CJ3, Grob SPn Utility Jet.FJ44-3A-24 AC-F 1, 3, 1 1, 2 An 2,400 lb. t. — — 23 48 — Cessna Citation CJ2+.FJ44-3AP AC-F 1, 3, 1 1, 2 An 3,050 lb. t. — — 23 48 — Piper Jet.FJ44-4A AC-F 1, 3, 1 1, 2 An 3,500 lb. t. — — 25.3 52.8 — Cessna Citation CJ4.P8300-15 A-F 2, 5 2 An 1,500 lb. t. — — 13.5 27.5 — DASA Taurus missiles.WJ24-8F AC-J 1, 1 1 An 240 lb. t. 1.2 — 10.8 19.5 50 Northrop BQM-74E target.WJ24-8G AC-J 1, 1 1 An 300 lb. t. — — 10.8 19.5 — Northrop BQM-74E target.WJ119-2 A-J 6 1 An 105 lb. t. — — 7 — — Missile applications.WTS117 C-S 1 1 An 125 shp. 0.69 — 12.9 20.9 72 Canadair CL-327.



NO

.OF

FAN

/CO

MPR

ESSI

ON

STA

GES

NO

.OF

TURB

INE

STAG

ES(H

P./

LP.)

COM

BUST

ION

TYP

E

MAX

.PO

WER

AT

SEA

LEVE

L(L

B.-T

HRUS

TO

RSH

P.)

SPEC

IFIC

FUE

LCO

NSU

MP-

TIO

NA

TM

AX.P

OW

ERLB

./LB

F.-HR

.or

LB./

HP.-H

R.

OVE

RALL

PRE

SSUR

ERA

TIO

AT

MAX

.PO

WER

MAX

.EN

VELO

PEDI

A.(I

N.)

MAX

.EN

VELO

PELE

NGT

H(IN

.)

DRY

WEI

GHT

LESS

TAIL

PIPE

(LB.

)



WORLD MILITARY




Abbreviations: A/B—with afterburner; eshp.—equivalent shaft horsepower; lb. t.—pounds-thrust; shp.—shaft horsepower.Footnotes: 1Weight includes speed reduction gearbox. 2Specific fuel consumption for RR commercial engines measured at cruise power. 3Fan tip diameter. 4Includes tailpipe. 5Installed weight; Pegasus has no tailpipe. 6Specific fuel consumption values for CFM56 engines are the specification values. 7Rated performance defined at ISA +30° C.

END OF TABLE

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